add ecaa9, techpod, flappy, blackbird

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Brian Delhaisse committed 2019-05-12 07:16:41 +02:00
1 parent 41927eb606
commit 763fd8d8d4
61 files changed
+7981 -21

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+6 -6
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@@ -305,7 +305,7 @@ class Body(object):
# just create setter
def _set_force(self, force):
"""Set the given force (expressed in the world cartesian frame) on the center of mass of the body."""
self.apply_force(link_id=-1, force=force, position=None, frame=Simulator.WORLD_FRAME)
self.apply_external_force(link_id=-1, force=force, position=None, frame=Simulator.WORLD_FRAME)
force = property(fset=_set_force)
@@ -322,7 +322,7 @@ class Body(object):
"""
self.sim.change_visual_shape(object_id=self.id, link_id=link_id, rgba_color=color)
def apply_force(self, link_id=-1, force=(0., 0., 0.), position=None, frame=Simulator.LINK_FRAME):
def apply_external_force(self, force=(0., 0., 0.), link_id=-1, position=None, frame=Simulator.LINK_FRAME):
"""
Apply the given force on the specified link of the current body.
@@ -331,17 +331,17 @@ class Body(object):
- this does not work when using `sim.setRealTimeSimulation(1)`.
Args:
link_id (int): link id to apply the force, if -1 it will apply the force on the base
force (np.array[3]): Cartesian forces to be applied on the body
link_id (int): link id to apply the force, if -1 it will apply the force on the base
position (np.array[3], None): position on the link where the force is applied (expressed in the given
cartesian frame, see next attribute :attr:`frame`). If None, it is the center of mass of the body
(or the link if specified).
frame (int): allows to specify the coordinate system of force/position. sim.LINK_FRAME (=1) for local
link frame, and sim.WORLD_FRAME (=2) for world frame. By default, it is the world frame.
"""
self.sim.apply_external_force(self.id, link_id, force, position, frame)
self.sim.apply_external_force(body_id=self.id, link_id=link_id, force=force, position=position, frame=frame)
def apply_external_torque(self, link_id=-1, torque=(0., 0., 0.), frame=Simulator.LINK_FRAME):
def apply_external_torque(self, torque=(0., 0., 0.), link_id=-1, frame=Simulator.LINK_FRAME):
"""
Apply an external torque on the body, or a link of the body. Note that after each simulation step, the external
torques are cleared to 0.
@@ -349,8 +349,8 @@ class Body(object):
Warnings: This does not work when using `sim.setRealTimeSimulation(1)`.
Args:
link_id (int): link id to apply the torque, if -1 it will apply the torque on the base
torque (float[3]): Cartesian torques to be applied on the body
link_id (int): link id to apply the torque, if -1 it will apply the torque on the base
frame (int): Specify the coordinate system of force/position: either `pybullet.WORLD_FRAME` (=2) for
Cartesian world coordinates or `pybullet.LINK_FRAME` (=1) for local link coordinates.
"""
+2 -2
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@@ -45,14 +45,14 @@ class Crab(HexapodRobot):
self.legs = [[self.get_link_ids(link) for link in links if link in self.link_names]
for links in [['coxa_l1', 'femur_l1', 'tibia_l1'],
[ 'coxa_r1', 'femur_r1', 'tibia_r1'],
['coxa_r1', 'femur_r1', 'tibia_r1'],
['coxa_l2', 'femur_l2', 'tibia_l2'],
['coxa_r2', 'femur_r2', 'tibia_r2'],
['coxa_l3', 'femur_l3', 'tibia_l3'],
['coxa_r3', 'femur_r3', 'tibia_r3']]]
self.feet = [self.get_link_ids(link) for link in ['tibia_foot_l1', 'tibia_foot_r1', 'tibia_foot_l2',
'tibia_foot_r2', 'tibia_foot_l3', 'tibia_foot_r3']
'tibia_foot_r2', 'tibia_foot_l3', 'tibia_foot_r3']
if link in self.link_names]
+159
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@@ -0,0 +1,159 @@
#!/usr/bin/env python
"""Provide the ECA A9 autonomous underwater vehicle platform.
"""
import os
import numpy as np
from pyrobolearn.robots.uuv import UUVRobot
__author__ = "Brian Delhaisse"
__copyright__ = "Copyright 2018, PyRoboLearn"
__license__ = "MIT"
__version__ = "1.0.0"
__maintainer__ = "Brian Delhaisse"
__email__ = "briandelhaisse@gmail.com"
__status__ = "Development"
# TODO: fix inertia tags in the URDF file
# TODO: several methods need to be moved to the `uuv.py` file.
class ECAA9(UUVRobot):
r"""Autonomous Unmanned Underwater Vehicle A9 from the ECA group
WARNING: Currently, pybullet does not simulate fluids, so we simulate the thrust, drag, buoyancy, lift, and weight
forces acting on the body. The gravity/weight force is simulated by pybullet.
The various forces are given by [3,4]:
1. The gravity/weight force is due to the attraction pull of the Earth is given by:
.. math:: F_g = m g
where :math:`m` is the mass of the object, and :math:`g` is the gravity constant (which is around
:math:`9.81 m/s^2` on the earth).
2. The buoyancy force is given by:
.. math:: F_b = \rho g V
where :math:`\rho` is the fluid density, :math:`g` is the gravity constant, and `V` is the volume of the
body submerged in the fluid.
3. The thrust force is due to the engine/motor/propeller of the object:
.. math:: F_t = \dot{m}_e v_e - \dot{m}_0 v_0 + (p_e - p_0) A_e
where :math:`\dot{m} = \rho A v` is the mass flow rate (i.e. mass/time), :math:`\rho` is the fluid density,
:math:`v` is the velocity, :math:`A` is the area where its normal is parallel to fluid flow, :math:`p` is the
pressure. The indices :math:`e` and :math:`0` stands for the exit and free stream (at the front of the submarine).
4. The lift force is given by:
.. math:: F_l = 1/2 C_l \rho A v^2
where :math:`C_l` is the lift coefficient at the desired angle of attack, :math:`A` is the platform area, \rho is
the fluid density, and :math:`v` is the velocity.
5. The drag force (which is opposed to the movement) is given by:
.. math:: F_d = 1/2 C_d \rho A v^2
where :math:`C_d` is the drag coefficient which is depending on the shape of the object, friction and viscosity
of the fluid, :math:`\rho` is the fluid density, :math:`A` is the platform area, and :math:`v` is the velocity.
For a submarine, the coefficient is approximately around 0.04 (see [3]).
References:
[1] https://www.ecagroup.com/en/solutions/a9-s-auv-autonomous-underwater-vehicle
[2] UUV Simulator: https://uuvsimulator.github.io/
[3] Aerodynamics (Nasa - check for equation): https://www.grc.nasa.gov/www/k-12/airplane/short.html
[4] https://s2.smu.edu/propulsion/Pages/navigation.htm
[5] Introduction to Ocean Waves: http://pordlabs.ucsd.edu/rsalmon/111.textbook.pdf
[6] https://fenicsproject.org/
"""
def __init__(self, simulator, position=(0, 0, 1.), orientation=(0, 0, 0, 1), fixed_base=False, scaling=1.,
urdf_path=os.path.dirname(__file__) + '/urdfs/ecaa9/eca_a9.urdf'):
# check parameters
if position is None:
position = (0., 0., 1.)
if len(position) == 2: # assume x, y are given
position = tuple(position) + (1.,)
if orientation is None:
orientation = (0, 0, 0, 1)
if fixed_base is None:
fixed_base = False
super(ECAA9, self).__init__(simulator, urdf_path, position, orientation, fixed_base, scaling)
self.name = 'eca_a9'
self.volume = 0.0679998770412 * scaling**3 # from urdf
self.sea_water_density = 1027
self.center_buoyancy = np.array([0.000106, 0., 0.6]) # from urdf
def calculate_buoyancy_force(self, fluid_density=None, g=9.81):
r"""
Calculate the buoyancy force.
Args:
fluid_density (float, None): density of the fluid [kg/m^3]
g (gravity): gravity value in the z direction.
Returns:
np.array[3]: buoyancy force
"""
# currently, we assume that the whole body is submerged in the
if fluid_density is None:
fluid_density = self.sea_water_density
return fluid_density * g * self.volume * np.array([0., 0., 1.])
# TODO: add `fill_tank(volume)` and `empty_tank(volume)`
def add_mass(self, mass=0., local_inertia_diagonal=(0., 0., 0.)):
r"""
Add mass to the submarine; a submarine has multiple ballast/trim tanks to control its buoyancy. This is
only valid in the simulator.
Args:
mass (float): mass that will be added to the base link.
local_inertia_diagonal (np.array[3]): local inertia diagonal around the CoM of the base link.
"""
info = self.sim.get_dynamics_info(body_id=self.id, link_id=-1)
mass += info[0]
local_inertia_diagonal = np.array(local_inertia_diagonal) + np.array(info[2])
self.sim.change_dynamics(body_id=self.id, link_id=-1, mass=mass, local_inertia_diagonal=local_inertia_diagonal)
# Test
if __name__ == "__main__":
from itertools import count
from pyrobolearn.simulators import BulletSim
from pyrobolearn.worlds import BasicWorld
# Create simulator
sim = BulletSim()
# create world
world = BasicWorld(sim)
# create robot
robot = ECAA9(sim)
# print information about the robot
robot.print_info()
fb = robot.calculate_buoyancy_force()
robot.add_mass(0.05)
# robot.add_joint_slider(range(5))
# robot.change_transparency(alpha=1.)
# run simulation
for i in count():
pos = robot.get_base_position()
# apply force in the simulation
robot.apply_external_force(force=fb, link_id=-1, position=pos+robot.center_buoyancy,
frame=BulletSim.WORLD_FRAME)
# robot.update_joint_slider()
# robot.set_joint_velocities([10], [4])
# step in simulation
world.step(sleep_dt=1./240)
+433
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@@ -0,0 +1,433 @@
#!/usr/bin/env python
"""Provide the techpod platform.
"""
import os
import json
import numpy as np
from pyrobolearn.robots.uav import FlappingWingUAV
__author__ = "Brian Delhaisse"
__copyright__ = "Copyright 2018, PyRoboLearn"
__credits__ = "Fei et al."
__license__ = "MIT"
__version__ = "1.0.0"
__maintainer__ = "Brian Delhaisse"
__email__ = "briandelhaisse@gmail.com"
__status__ = "Development"
class SimpleNamespace:
"""A simple object subclass that provides attribute access to its namespace, as well as a meaningful repr.
Taken from: https://docs.python.org/3/library/types.html
"""
def __init__(self, **kwargs):
self.__dict__.update(kwargs)
def __repr__(self):
keys = sorted(self.__dict__)
items = ("{}={!r}".format(k, self.__dict__[k]) for k in keys)
return "{}({})".format(type(self).__name__, ", ".join(items))
def __eq__(self, other):
return self.__dict__ == other.__dict__
class Wing(object):
r"""Wing
Python code translated from C++ code provided in [1].
References:
[1] https://github.com/purdue-biorobotics/flappy/blob/master/flappy/envs/Wing.cpp
[2] "Flappy Hummingbird: An Open Source Dynamic Simulation of Flapping Wing Robots and Animals", Fei et al.,
2019
"""
def __init__(self, wing_index, wing_length, mean_chord, r33, r22, r11, r00, z_cp2, z_cp1, z_cp0, z_rd,
shoulder_width, stroke_plane_offset):
r"""
Initialize the wing and compute the dynamics on it.
Args:
wing_index (int): wing index (0 or 1). This is used to determine the sign of the axis for the motors.
Set it to 0 for the left wing, and 1 for the right wing.
wing_length (float): length of wing.
mean_chord (float): mean of the chord. "In aeronautics, a chord is the imaginary straight line joining the
leading and trailing edges of an aerofoil. The chord length is the distance between the trailing edge
and the point on the leading edge where the chord intersects the leading edge." (from Wikipedia)
r33 (float): wing geometry constant.
r22 (float): wing geometry constant.
r11 (float): wing geometry constant.
r00 (float): wing geometry constant.
z_cp2 (float): wing geometry constant.
z_cp1 (float): wing geometry constant.
z_cp0 (float): wing geometry constant.
z_rd (float): wing geometry constant.
shoulder_width (float): should width
stroke_plane_offset (float): stroke plane offset.
"""
self.air_density = 1.18009482370369
self.wing_index = wing_index
self.wing_length = wing_length
self.mean_chord = mean_chord
self.r33 = r33
self.r22 = r22
self.r11 = r11
self.r00 = r00
self.z_cp2 = z_cp2
self.z_cp1 = z_cp1
self.z_cp0 = z_cp0
self.z_rd = z_rd
self.sign = pow(-1, wing_index)
self.r_w = wing_length
self.d_0 = shoulder_width
self.d_s = stroke_plane_offset
self.r_cp = self.r_w * r33/r22 # span-wise center of pressure
# total force and moments
self.span_wise_center_of_pressure = 0
self.cord_wise_center_of_pressure = 0
self.normal_force = 0
self.aero_moment = 0
self.rotational_damping_moment = 0
# rotational damping moment coefficient
self.Crd = 5.0
def do_nothing(self):
# total force and moments
self.span_wise_center_of_pressure = 0
self.cord_wise_center_of_pressure = 0
self.normal_force = 0
self.aero_moment = 0
self.rotational_damping_moment = 0
def update_aero_force(self):
"""Update the aerodynamic forces applied on the wing; i.e. the normal force, aerodynamic moment and rotational
damping moment (the equations are provided in [2]).
"""
self.update_velocity_coefficients()
self.update_angle_of_attack()
self.CN = self.get_CN(self.alpha)
self.d_cp = self.get_center_of_pressure(self.alpha)
self.update_velocity_squared_coefficients()
# the normal force, aerodynamic moment and rotational damping moment are given in [2]
self.normal_force = 0.5 * self.air_density * self.mean_chord * self.CN * \
(self.a_u2 * self.r_w**3 * self.r22 + self.a_u1 * self.r_w**2 * self.r11 +
self.a_u0 * self.r_w * self.r00)
self.aero_moment = -0.5 * self.air_density * self.d_cp * self.CN * self.mean_chord**2 * \
(self.a_u2 * self.r_w**3 * self.z_cp2 + self.a_u1 * self.r_w**2 * self.z_cp1 +
self.a_u0 * self.r_w * self.z_cp0)
if self.normal_force != 0:
self.cord_wise_center_of_pressure = -self.aero_moment / self.normal_force
else:
self.cord_wise_center_of_pressure = 0
self.span_wise_center_of_pressure = self.r_cp
self.rotational_damping_moment = -0.125 * self.air_density * np.abs(self.dtheta) * self.dtheta * self.Crd * \
self.r_w * self.mean_chord**4 * self.z_rd
def update_state(self, body_velocity_rpy, body_velocity, stroke_plane_angle, stroke_plane_velocity, stroke_angle,
stroke_velocity, deviation_angle, deviation_velocity, rotate_angle, rotate_velocity):
"""Update the state of the wing."""
self.velocity = body_velocity
self.drpy = body_velocity_rpy
# stroke plane
self.Phi = stroke_plane_angle
self.dPhi = stroke_plane_velocity
# stroke
self.psi = stroke_angle
self.dpsi = stroke_velocity
# deviation
self.phi = deviation_angle
self.dphi = deviation_velocity
# wing rotation
self.theta = rotate_angle
self.dtheta = rotate_velocity
# wing trigonometry pre calculation
self.s_Phi = np.sin(self.Phi)
self.c_Phi = np.cos(self.Phi)
self.s_psi = np.sin(self.psi)
self.c_psi = np.cos(self.psi)
self.s_phi = np.sin(self.phi)
self.c_phi = np.cos(self.phi)
def update_velocity_coefficients(self):
"""Update the velocity coefficients."""
u, v, w = self.velocity
p, q, r = self.drpy
s_Phi, c_Phi, s_psi, c_psi, s_phi, c_phi = self.s_Phi, self.c_Phi, self.s_psi, self.c_psi, self.s_phi, \
self.c_phi
dPhi, dpsi, dphi = self.dPhi, self.dpsi, self.dphi
d_0, d_s = self.d_0, self.d_s
# velocity coefficients
self.u_o1 = self.sign * (p * c_psi * c_Phi - dPhi * s_psi) + (q * s_psi + r * c_psi * s_Phi + dphi)
self.u_o0 = self.sign * (-(u + q * d_s) * c_phi * s_Phi - r * d_0 * s_phi * s_psi * c_Phi - (v - p * d_s) *
s_phi * c_psi + w * s_phi * s_psi * s_Phi + p * d_0 * c_phi * c_Phi) + \
((u + q * d_s) * s_phi * s_psi * c_Phi + r * d_0 * c_phi * s_Phi + w * c_phi * c_Phi + p * d_0 *
s_phi * s_psi * s_Phi)
self.u_i1 = self.sign * (p * s_phi * s_psi * c_Phi + r * c_phi * c_Phi + dPhi * s_phi * c_psi) + \
(-p * c_phi * s_Phi - q * s_phi * c_psi + r * s_phi * s_psi * s_Phi + dpsi * c_phi)
self.u_i0 = self.sign * (r * d_0 * c_psi * c_Phi - (v - p * d_s) * s_psi - w * c_psi * s_Phi) + \
(-(u + q * d_s) * c_psi * c_Phi - p * d_0 * c_psi * s_Phi)
def update_angle_of_attack(self):
"""Update the angle of attack (AoA)."""
# AoA correction double
self.u_i = self.u_i1 * self.r_cp + self.u_i0
if self.u_i != 0:
self.delta_alpha = np.arctan((self.u_o1 * self.r_cp + self.u_o0) / (self.u_i1 * self.r_cp + self.u_i0))
else:
self.delta_alpha = 0
# geometric AoA
self.alpha_0 = self.theta + np.double(np.sign(self.u_i)) * np.pi / 2
self.alpha = self.alpha_0 - self.delta_alpha
@staticmethod
def get_CN(alpha):
# see equation (8) in paper [2]
return 1.8 * np.sin(2 * alpha) * np.cos(alpha) + 1.95 * np.sin(alpha) - 1.5 * np.cos(2 * alpha) * np.sin(alpha)
@staticmethod
def get_center_of_pressure(alpha):
return 0.46 - 0.332 * np.cos(alpha) - 0.037 * np.cos(3 * alpha) - 0.013 * np.cos(5 * alpha)
def update_velocity_squared_coefficients(self):
# velocity squared coefficients
self.a_u2 = self.u_i1**2 + self.u_o1**2
self.a_u1 = 2 * self.u_i1 * self.u_i0 + 2 * self.u_o1 * self.u_o0
self.a_u0 = self.u_i0**2 + self.u_o0**2
class Actuator:
r"""Actuator
Code copied-pasted from [1] (I didn't change anything except adding some whitespaces).
References:
[1] https://github.com/purdue-biorobotics/flappy/blob/master/flappy/envs/Wing.cpp
[2] "Flappy Hummingbird: An Open Source Dynamic Simulation of Flapping Wing Robots and Animals", Fei et al.,
2019
"""
def __init__(self, motor_properties):
config = SimpleNamespace(**motor_properties)
self.resistance = config.resistance
self.torque_constant = config.torque_constant
self.gear_ratio = config.gear_ratio
self.mechanical_efficiency = config.mechanical_efficiency
self.friction_coefficient = config.friction_coefficient
self.damping_coefficient = config.damping_coefficient
self.inertia = config.inertia
self.inertia_torque = 0
self.damping_torque = 0
self.friction_torque = 0
self.magnetic_torque = 0
self.motor_torque = 0
self.voltage = 0
self.current = 0
self.back_EMF = 0
self.output_torque = 0
self.config = config
self.reset()
def update_driver_voltage(self, voltage):
self.voltage = voltage
def update_torque(self, stroke_velocity, stroke_acceleration):
psi_dot = stroke_velocity
psi_ddot = stroke_acceleration
motor_vel = psi_dot * self.gear_ratio
motor_accel = psi_ddot * self.gear_ratio
if psi_dot > 0:
sign = 1
elif psi_dot < 0:
sign = -1
else:
sign = 0
self.back_EMF = self.torque_constant * motor_vel
self.current = (self.voltage - self.back_EMF) / self.resistance
self.inertia_torque = self.inertia * motor_accel
self.damping_torque = self.damping_coefficient * motor_vel
self.friction_torque = self.friction_coefficient * sign
self.magnetic_torque = self.torque_constant * self.current
self.motor_torque = self.magnetic_torque - self.inertia_torque - self.damping_torque - self.friction_torque
self.output_torque = self.motor_torque * self.gear_ratio * self.mechanical_efficiency
def get_torque(self):
return self.output_torque
def reset(self):
self.inertia_torque = 0
self.damping_torque = 0
self.friction_torque = 0
self.magnetic_torque = 0
self.motor_torque = 0
self.current = 0
self.back_EMF = 0
self.output_torque = 0
class Flappy(FlappingWingUAV):
r"""Flappy Hummingbird UAV (from Purdue University)
This is the main class for the flappy hummingbird (a flapping wing micro aerial vehicle (FWMAV)). Most of the code
as well as the URDF model comes from [2,3].
The flappy hummingbird has 2 wings and each one has 2 degrees of freedom; the stroke and rotation angles.
Warnings: Currently, in pybullet there is no air, so we simulate all the forces acting on the flappy vehicle as
described in the paper and code [2,3]. The gravity is carried out by pybullet.
References:
[1] "Design Optimization and System Integration of Robotic Hummingbird", 2017, Zhang et al.
[2] "Flappy Hummingbird: An Open Source Dynamic Simulation of Flapping Wing Robots and Animals", Fei et al.,
2019
[3] https://github.com/purdue-biorobotics/flappy
"""
def __init__(self, simulator, position=(0, 0, 0.5), orientation=(0, 0, 0, 1), fixed_base=False, scaling=1.,
urdf=os.path.dirname(__file__) + '/urdfs/flappy/flappy.urdf',
config=os.path.dirname(__file__) + '/urdfs/flappy/config/mav_config.json'):
super(Flappy, self).__init__(simulator, urdf, position, orientation, fixed_base)
with open(config) as f:
config = json.load(f)[0]
config = SimpleNamespace(**config)
# create wings
self.left_wing = Wing(0, config.wing_length, config.mean_chord, config.r33, config.r22, config.r11, config.r00,
config.z_cp2, config.z_cp1, config.z_cp0, config.z_rd, config.left_shoulder_width,
config.stroke_plane_offset)
self.right_wing = Wing(1, config.wing_length, config.mean_chord, config.r33, config.r22, config.r11, config.r00,
config.z_cp2, config.z_cp1, config.z_cp0, config.z_rd, config.right_shoulder_width,
config.stroke_plane_offset)
# create motors
self.left_motor = Actuator(config.left_motor_properties)
self.right_motor = Actuator(config.right_motor_properties)
# joints
self.left_wing_joints = [self.get_link_ids(link) for link in ['left_leading_edge', 'left_wing']
if link in self.link_names]
self.right_wing_joints = [self.get_link_ids(link) for link in ['right_leading_edge', 'right_wing']
if link in self.link_names]
self.wings = [self.left_wing_joints, self.right_wing_joints]
# joints = [left stroke, left rotate, right stroke, right rotate]
self.wing_joints = self.left_wing_joints + self.right_wing_joints
# dummy variables for now
# self.driver_update_time = 0
# self.dt_driver = 1./1e3
self.prev_t = None
self.prev_joint_velocities = None
def apply_voltage(self, t, input_voltage): # step(self, t, input_voltage):
# get the joint positions for the left and right wing joints
joint_positions = self.get_joint_positions(self.wing_joints)
joint_velocities = self.get_joint_velocities(self.wing_joints)
# joint_accelerations = self.get_joint_accelerations(self.wing_joints)
if self.prev_t is None:
joint_accelerations = np.zeros(len(self.wing_joints))
else:
joint_accelerations = (joint_velocities - self.prev_joint_velocities) / (t - self.prev_t)
# update aerodynamic forces
self.left_wing.update_state(self.angular_velocity, self.linear_velocity, 0, 0, joint_positions[0],
joint_velocities[0], 0, 0, joint_positions[1], joint_velocities[1])
self.right_wing.update_state(self.angular_velocity, self.linear_velocity, 0, 0, joint_positions[2],
joint_velocities[2], 0, 0, joint_positions[3], joint_velocities[3])
self.left_wing.update_aero_force()
self.right_wing.update_aero_force()
# update voltage
# if t >= self.driver_update_time:
# self.driver_update_time += self.dt_driver
self.left_motor.update_driver_voltage(input_voltage[0])
self.right_motor.update_driver_voltage(input_voltage[1])
# update torque (left and right strokes)
self.left_motor.update_torque(joint_velocities[0], joint_accelerations[0])
self.right_motor.update_torque(joint_velocities[2], joint_accelerations[2])
# apply stroke torque
torques = np.zeros(self.num_dofs)
torques[0] = self.left_motor.get_torque()
torques[2] = self.right_motor.get_torque()
self.set_joint_torques(torques)
# get aero forces
left_normal_force = np.array([self.left_wing.normal_force, 0, 0]) # in wing x direction
right_normal_force = np.array([self.right_wing.normal_force, 0, 0])
left_cop = np.array([0, self.left_wing.span_wise_center_of_pressure,
(-1) * self.left_wing.cord_wise_center_of_pressure])
right_cop = np.array([0, (-1) * self.right_wing.span_wise_center_of_pressure,
(-1) * self.right_wing.cord_wise_center_of_pressure])
left_rot_damping_moment = np.array([0, self.left_wing.rotational_damping_moment, 0]) # in wing y direction
right_rot_damping_moment = np.array([0, self.right_wing.rotational_damping_moment, 0])
# apply aero force and moment on wing
# self.apply_external_force(left_normal_force, link_id=1, position=left_cop, frame=BulletSim.LINK_FRAME)
# self.apply_external_force(right_normal_force, link_id=3, position=right_cop, frame=BulletSim.LINK_FRAME)
# self.apply_external_torque(left_rot_damping_moment, link_id=1, frame=BulletSim.LINK_FRAME)
# self.apply_external_torque(right_rot_damping_moment, link_id=3, frame=BulletSim.LINK_FRAME)
# save
self.prev_t = t
self.prev_joint_velocities = joint_velocities
# Test
if __name__ == "__main__":
import time
from itertools import count
from pyrobolearn.simulators import BulletSim
from pyrobolearn.worlds import BasicWorld
# Create simulator
sim = BulletSim()
# create world
world = BasicWorld(sim)
# create robot
robot = Flappy(sim)
# print information about the robot
robot.print_info()
robot.add_joint_slider(robot.left_wing_joints)
# run simulation
for i in count():
robot.update_joint_slider()
# signal = 3 * np.sin(2. * np.pi * i/1000) * np.ones(2)
# robot.apply_voltage(time.time(), signal)
# robot.set_joint_positions(1. * np.sin(2 * np.pi * i/240), joint_ids=0)
# step in simulation
world.step(sleep_dt=1./240)
+11 -11
View File
@@ -18,12 +18,13 @@ __email__ = "briandelhaisse@gmail.com"
__status__ = "Development"
# TODO: several methods such as the calculation of the thrust force should be done in `uav.py` file, not here
class Quadcopter(RotaryWingUAV):
r"""Quadcopter
WARNING: Currently, in pybullet there is no air, so we simulate the thrust force.
Based on momentum theory, we can calculate the thrust [4,5,6] to be:
Based on momentum theory, we can calculate the thrust [5,6,7] to be:
.. math::
@@ -56,9 +57,9 @@ class Quadcopter(RotaryWingUAV):
[3] https://github.com/prfraanje/quadcopter_sim
[4] https://github.com/ethz-asl/rotors_simulator
[4] "Propeller Thrust" (NASA): https://www.grc.nasa.gov/WWW/K-12/airplane/propth.html
[5] "Static thrust calculation": https://quadcopterproject.wordpress.com/static-thrust-calculation/
[6] "Propeller Static & Dynamic Thrust Calculation":
[5] "Propeller Thrust" (NASA): https://www.grc.nasa.gov/WWW/K-12/airplane/propth.html
[6] "Static thrust calculation": https://quadcopterproject.wordpress.com/static-thrust-calculation/
[7] "Propeller Static & Dynamic Thrust Calculation":
https://www.electricrcaircraftguy.com/2013/09/propeller-static-dynamic-thrust-equation.html
https://www.electricrcaircraftguy.com/2014/04/propeller-static-dynamic-thrust-equation-background.html
"""
@@ -133,14 +134,13 @@ class Quadcopter(RotaryWingUAV):
diameter = (4. * area / np.pi)**0.5
return air_density * area * (tmp**2 - tmp*v0) * (self.k1 * diameter / propeller_pitch)**self.k2
def set_joint_velocities(self, velocities, joint_ids=None, max_velocity=True, forces=True):
def set_propeller_velocities(self, velocities, max_velocity=True, forces=True):
"""
Set the joint velocities and apply the thrust force on the propeller link corresponding to the given
joint id(s).
Args:
velocities (float[4]): velocity of each propeller
joint_ids (int[4], None): Not used here
velocities (np.array[4]): velocity of each propeller
forces (float, np.float[N], None, bool): maximum motor torques / forces. If True, it will apply the
default maximum force values.
max_velocity (float, bool, None): if True, it will make sure that the given velocity(ies) are below their
@@ -156,7 +156,7 @@ class Quadcopter(RotaryWingUAV):
joint_ids = self.joints
# call parent method
super(Quadcopter, self).set_joint_velocities(velocities, joint_ids, max_velocity, forces)
super(Quadcopter, self).set_joint_velocities(velocities, joint_ids, forces, max_velocity)
# calculate thrust force of the given joints, and apply it on the link
for jnt, d, v in zip(joint_ids, self.turning_directions, velocities):
@@ -165,7 +165,7 @@ class Quadcopter(RotaryWingUAV):
# compute propeller speed v0
state = self.sim.get_link_state(self.id, jnt, compute_velocity=True) # , compute_forward_kinematics=True)
R = np.array(get_matrix_from_quaternion(state[1]))
R = get_matrix_from_quaternion(state[1])
linear_velocity = np.array(state[-2])
propeller_up_vec = R.dot(np.array([0., 0., 1.]))
v0 = linear_velocity.dot(propeller_up_vec)
@@ -176,7 +176,7 @@ class Quadcopter(RotaryWingUAV):
# f = self.mass * self.gravity / 4.
# apply force in the simulation
self.apply_external_force([0, 0, f], jnt, position=(0., 0., 0.))
self.apply_external_force(force=[0, 0, f], link_id=jnt, position=(0., 0., 0.))
def get_stationary_joint_velocity(self):
fg = self.mass * self.gravity / 4.
@@ -217,6 +217,6 @@ if __name__ == "__main__":
# run simulation
for i in count():
robot.set_joint_velocities(v)
robot.set_propeller_velocities(v)
# step in simulation
world.step(sleep_dt=1./240)
+6
View File
@@ -2129,9 +2129,15 @@ class Robot(ControllableBody):
# compute and return joint accelerations
torques = np.array(torques)
if not self.fixed_base: # if floating base
torques = np.concatenate((np.zeros(6), torques))
Hinv = np.linalg.inv(self.get_mass_matrix(q))
C = self.calculate_inverse_dynamics(np.zeros(len(q)), dq=dq, q=q)
if np.any(np.equal(C, None)):
C = np.zeros(len(torques))
acc = Hinv.dot(torques - C)
if not self.fixed_base: # if floating base
return acc[6:]
return acc
def get_mass_matrix(self, q=None, q_idx=None):
+255
View File
@@ -0,0 +1,255 @@
#!/usr/bin/env python
"""Provide the techpod platform.
"""
import os
import numpy as np
from pyrobolearn.robots.uav import FixedWingUAV
from pyrobolearn.utils.transformation import get_matrix_from_quaternion
from pyrobolearn.utils.units import inches_to_meters
__author__ = "Brian Delhaisse"
__copyright__ = "Copyright 2018, PyRoboLearn"
__license__ = "MIT"
__version__ = "1.0.0"
__maintainer__ = "Brian Delhaisse"
__email__ = "briandelhaisse@gmail.com"
__status__ = "Development"
# TODO: several methods have to be moved in the `uav.py` file.
class Techpod(FixedWingUAV):
r"""Techpod UAV
Four forces (thrust, lift, drag, and gravity) act on an airplane.
WARNING: Currently, in pybullet there is no air, so we simulate the lift, thrust, and drag forces. The gravity
is carried out by pybullet.
References:
[1] https://github.com/ethz-asl/rotors_simulator
[2] "Theory of flight": web.mit.edu/16.00/www/aec/flight.html
[3] "NASA: Guided Tours of the BGA": www.grc.nasa.gov/WWW/k-12/airplane/guided.html
"""
def __init__(self,
simulator,
position=(0, 0, 0.5),
orientation=(0, 0, 0, 1),
fixed_base=False,
scaling=1.,
urdf=os.path.dirname(__file__) + '/urdfs/techpod/techpod.urdf'):
# check parameters
if position is None:
position = (0., 0., 0.5)
if len(position) == 2: # assume x, y are given
position = tuple(position) + (0.5,)
if orientation is None:
orientation = (0, 0, 0, 1)
if fixed_base is None:
fixed_base = False
super(Techpod, self).__init__(simulator, urdf, position, orientation, fixed_base, scaling)
self.name = 'techpod'
# info
self.gravity = 9.81
self.air_density = 1.225
# change dynamics
self.sim.change_dynamics(body_id=self.id, link_id=0, lateral_friction=0.)
# from urdf
self.radius = 0.15 # 0.14
self.diameter = 2. * self.radius
self.area = np.pi * self.radius**2
self.max_velocity = 770 # rad/sec
# Propeller pitches are around 0.0762m (3 inches) and 0.127m (5 inches)
# (from https://www.dronezon.com/learn-about-drones-quadcopters/how-a-quadcopter-works-with-propellers-and\
# -motors-direction-design-explained/)
# The larger the prop (either increasing diameter, or pitch or both), the more energy it takes to spin it.
# When buying propellers, they follow the syntax `LxP` where `L` is the length/diameter of the propeller
# (in inches) and `P` is the propeller pitch (also in inches).
# 1 inch = 0.0254m --> 0.28m = 11 inches
# The value of the pitch below has been set by looking online for quadcopter props with 11 inches of length
self.propeller_pitch = inches_to_meters(7) # 4.7) # inches_to_meters(5.)
# some constants
self.k1 = 1./3.29546
self.k2 = 1.5
def calculate_thrust_force(self, angular_speed, area, propeller_pitch, v0=0, air_density=1.225):
r"""
Calculate the thrust force generated by the propeller (based on [6]).
Args:
angular_speed (float): angular speed of the propeller [rad/s]. If RPM, convert it to rad/s using the
formula :math:`1 RPM = \frac{2\pi}{60} rad/s`.
area (float): area of the propeller [m^2]
propeller_pitch (float): "distance a propeller would move in 1 revolution if it were moving through a
soft solid" [m]
air_density (float): density of air [kg/m^3]. By default, it is the density of the air at sea level and at
15 degrees Celsius. Note that this varies with the temperature, humidity, and pressure. It decreases
with increasing altitude.
Returns:
float: thrust force generated by the propeller [N]
References:
[1] "Thrust Equation": https://www.grc.nasa.gov/WWW/k-12/airplane/thrsteq.html
[2] "Propeller Thrust": https://www.grc.nasa.gov/WWW/k-12/airplane/propth.html
[3] "Propeller Analysis": https://www.grc.nasa.gov/WWW/k-12/airplane/propanl.html
"""
tmp = angular_speed / (2*np.pi) * propeller_pitch
diameter = (4. * area / np.pi)**0.5
return air_density * area * (tmp**2 - tmp*v0) * (self.k1 * diameter / propeller_pitch)**self.k2
def calculate_lift_force(self):
r"""
Calculate the lift force.
Returns:
float[3]: lift force (in the z direction)
References:
[1] "What is Lift?": https://www.grc.nasa.gov/WWW/k-12/airplane/lift1.html
[2] "Lift Equation": https://www.grc.nasa.gov/WWW/k-12/airplane/lifteq.html
[3] "Inclination Effects on Lift": https://www.grc.nasa.gov/WWW/k-12/airplane/incline.html
[4] https://www.comsol.com/blogs/how-do-i-compute-lift-and-drag/
"""
pass
def calculate_drag_force(self):
r"""
Calculate the drag force.
Returns:
float[3]: drag force (in the -x direction)
References:
[1] "What is Drag?": https://www.grc.nasa.gov/WWW/k-12/airplane/drag1.html
[2] "Drag Equation": https://www.grc.nasa.gov/WWW/k-12/airplane/drageq.html
[3] https://www.comsol.com/blogs/how-do-i-compute-lift-and-drag/
"""
pass
def calculate_elevator_moment(self):
r"""
Calculate the moment due to the elevators [1].
Returns:
float[3]: resulting moment in the y direction
Reference:
[1] "Horizontal Stabilizer - Elevator": https://www.grc.nasa.gov/WWW/k-12/airplane/elv.html
[2] "Aircraft Rotations": https://www.grc.nasa.gov/WWW/k-12/airplane/rotations.html
"""
pass
def calculate_aileron_moment(self):
"""
Calculate the moment due to the ailerons that increases/decreases the lift force [1].
Returns:
float[3]: resulting moment in the x direction.
References:
[1] "Ailerons": https://www.grc.nasa.gov/WWW/k-12/airplane/alr.html
[2] "Aircraft Rotations": https://www.grc.nasa.gov/WWW/k-12/airplane/rotations.html
"""
pass
def calculate_flap_moment(self):
"""
Increase lift or drag.
Returns:
References:
[1] "Flaps and Slats": https://www.grc.nasa.gov/WWW/k-12/airplane/flap.html
"""
pass
def calculate_rudder_moment(self):
"""
Calculate the moment due to the rudder [1].
Returns:
float[3]: resulting moment (in the z direction)
Reference:
[1] "Vertical Stabilizer - Rudder": https://www.grc.nasa.gov/WWW/k-12/airplane/rud.html
[2] "Aircraft Rotations": https://www.grc.nasa.gov/WWW/k-12/airplane/rotations.html
"""
pass
def set_propeller_velocities(self, velocities, max_velocity=True, forces=True):
"""
Set the joint velocities and apply the thrust force on the propeller link corresponding to the given
joint id(s).
Args:
velocities (float[4]): velocity of each propeller
forces (float, np.float[N], None, bool): maximum motor torques / forces. If True, it will apply the
default maximum force values.
max_velocity (float, bool, None): if True, it will make sure that the given velocity(ies) are below their
authorized maximum value(s) (inferred from the URDF, or set previously by the user). If you already
did the check outside the method or if you don't want limits, set this variable to False.
Returns:
None
"""
joint_id = 7
# call parent method
super(Techpod, self).set_joint_velocities(velocities, joint_id, forces, max_velocity)
# calculate thrust force of the given joints, and apply it on the link
if max_velocity and velocities > self.max_velocity:
velocities = self.max_velocity
# compute propeller speed v0
state = self.sim.get_link_state(self.id, joint_id, compute_velocity=True) # , compute_forward_kinematics=True)
R = get_matrix_from_quaternion(state[1])
linear_velocity = np.array(state[-2])
propeller_up_vec = R.dot(np.array([0., 1., 0.]))
v0 = linear_velocity.dot(propeller_up_vec)
# v0 = 0 # static thrust
# compute thrust
f = self.calculate_thrust_force(velocities, self.area, self.propeller_pitch) # , v0)
# apply force in the simulation
# f = 20
self.apply_external_force(force=[0, 0, -f], link_id=joint_id, position=(0., 0., 0.))
def apply_physics(self):
pass
# Test
if __name__ == "__main__":
from itertools import count
from pyrobolearn.simulators import BulletSim
from pyrobolearn.worlds import BasicWorld
# Create simulator
sim = BulletSim()
# create world
world = BasicWorld(sim)
# create robot
robot = Techpod(sim)
# print information about the robot
robot.print_info()
# run simulation
for i in count():
robot.set_propeller_velocities(100)
# step in simulation
world.step(sleep_dt=1./240)
+15
View File
@@ -24,12 +24,18 @@ class UAVRobot(Robot):
super(UAVRobot, self).__init__(simulator, urdf, position, orientation, fixed_base, scale)
self.propellers = [] # list of propellers id
self.wings = [] # list of wing id
@property
def num_propellers(self):
"""Return the number of propellers"""
return len(self.propellers)
@property
def num_wings(self):
"""Return the number of wings."""
return len(self.wings)
class FixedWingUAV(UAVRobot):
r"""Fixed Wing Robot
@@ -47,3 +53,12 @@ class RotaryWingUAV(UAVRobot):
def __init__(self, simulator, urdf, position=None, orientation=None, fixed_base=False, scale=1.):
super(RotaryWingUAV, self).__init__(simulator, urdf, position, orientation, fixed_base, scale)
class FlappingWingUAV(UAVRobot):
r"""Flapping Wing Robot
"""
def __init__(self, simulator, urdf, position=None, orientation=None, fixed_base=False, scale=1.):
super(FlappingWingUAV, self).__init__(simulator, urdf, position, orientation, fixed_base, scale)
@@ -0,0 +1,340 @@
<?xml version="1.0"?>
<!-- created with Phobos 0.7 -->
<robot name="biped">
<material name = "black">
<color rgba="0.25 0.25 0.25 1.0"/>
</material>
<link name="l_ab_ad">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="0.8"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="l_yaw_motor">
<origin xyz="0 0 -0.04328" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.009.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="l_yaw_motor">
<origin xyz="0 0 -0.04328" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.009.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="l_foot">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="l_foot_mesh">
<origin xyz="0.00032 -0.02422 -0.0314" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.003.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="l_foot_mesh">
<origin xyz="0.00032 -0.02422 -0.0314" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.003.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="l_lower">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="1.0"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="l_leg_lower">
<origin xyz="0 -0.01638 -0.14422" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.001.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="l_leg_lower">
<origin xyz="0 -0.01638 -0.14422" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.001.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="l_upper">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="0.2"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="l_leg_upper">
<origin xyz="0 0.04702 -0.13046" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.005.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="l_leg_upper">
<origin xyz="0 0.04702 -0.13046" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.005.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="l_yaw">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="2.0"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="l_hip">
<origin xyz="0 0 0" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.007.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="l_hip">
<origin xyz="0 0 0" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.007.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="r_ab_ad">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="0.8"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="r_yaw_motor">
<origin xyz="0 0 -0.03098" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.010.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="r_yaw_motor">
<origin xyz="0 0 -0.03098" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.010.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="r_foot">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="r_foot_mesh">
<origin xyz="0.00039 -0.02422 -0.0314" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.004.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="r_foot_mesh">
<origin xyz="0.00039 -0.02422 -0.0314" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.004.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="r_lower">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="1.0"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
<visual name="r_leg_lower">
<origin xyz="0 -0.01638 -0.14422" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.002.stl" scale="0.1 0.1 0.1"/>
</geometry>
<material name="black"/>
</visual>
<collision name="r_leg_lower">
<origin xyz="0 -0.01638 -0.14422" rpy="0 0 0"/>
<geometry>
<mesh filename="meshes/V2Mockup.002.stl" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<link name="r_upper">
<inertial>
<origin xyz="0 0 0" rpy="0 0 0"/>
<mass value="0.2"/>
<inertia ixx="0.001" ixy="0" ixz="0" iyy="0.001" iyz="0" izz="0.001"/>
</inertial>
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<?xml version="1.0" encoding="utf-8"?>
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+293
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<?xml version="1.0" encoding="utf-8"?>
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+403
View File
@@ -0,0 +1,403 @@
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+406
View File
@@ -0,0 +1,406 @@
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</polylist>
</mesh>
</geometry>
</library_geometries>
<library_controllers/>
<library_visual_scenes>
<visual_scene id="Scene" name="Scene">
<node id="Camera" name="Camera" type="NODE">
<matrix sid="transform">0.6858805 -0.3173701 0.6548619 7.481132 0.7276338 0.3124686 -0.6106656 -6.50764 -0.01081678 0.8953432 0.4452454 5.343665 0 0 0 1</matrix>
<instance_camera url="#Camera-camera"/>
</node>
<node id="Lamp" name="Lamp" type="NODE">
<matrix sid="transform">-0.2908646 -0.7711008 0.5663932 4.076245 0.9551712 -0.1998834 0.2183912 1.005454 -0.05518906 0.6045247 0.7946723 5.903862 0 0 0 1</matrix>
<instance_light url="#Lamp-light"/>
</node>
<node id="scale" name="scale" type="NODE">
<matrix sid="transform">0.1 0 0 0 0 0.1 0 0 0 0 0.1 0 0 0 0 1</matrix>
<node id="Cylinder" name="Cylinder" type="NODE">
<matrix sid="transform">1 0 0 0 0 1 0 0 0 0 1 -0.475 0 0 0 1</matrix>
<instance_geometry url="#Cylinder_005-mesh" name="Cylinder">
<bind_material>
<technique_common>
<instance_material symbol="silver-material" target="#silver-material"/>
</technique_common>
</bind_material>
</instance_geometry>
</node>
<node id="Cylinder_001" name="Cylinder_001" type="NODE">
<matrix sid="transform">1 0 0 0 0 1 0 0 0 0 0.9419355 0.15 0 0 0 1</matrix>
<instance_geometry url="#Cylinder_001-mesh" name="Cylinder_001">
<bind_material>
<technique_common>
<instance_material symbol="silver-material" target="#silver-material"/>
</technique_common>
</bind_material>
</instance_geometry>
</node>
<node id="Cylinder_002" name="Cylinder_002" type="NODE">
<matrix sid="transform">1 0 0 0 0 1 0 0 0 0 1 -0.775 0 0 0 1</matrix>
<instance_geometry url="#Cylinder_002-mesh" name="Cylinder_002">
<bind_material>
<technique_common>
<instance_material symbol="black-material" target="#black-material"/>
</technique_common>
</bind_material>
</instance_geometry>
</node>
<node id="Cylinder_005" name="Cylinder_005" type="NODE">
<matrix sid="transform">1 0 0 0 0 1 0 0 0 0 1 0.625 0 0 0 1</matrix>
<instance_geometry url="#Cylinder_007-mesh" name="Cylinder_005">
<bind_material>
<technique_common>
<instance_material symbol="silver-material" target="#silver-material"/>
</technique_common>
</bind_material>
</instance_geometry>
</node>
<node id="Cylinder_004" name="Cylinder_004" type="NODE">
<matrix sid="transform">1 0 0 0 0 1 0 0 0 0 1 0.825 0 0 0 1</matrix>
<instance_geometry url="#Cylinder_006-mesh" name="Cylinder_004">
<bind_material>
<technique_common>
<instance_material symbol="black-material" target="#black-material"/>
</technique_common>
</bind_material>
</instance_geometry>
</node>
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</visual_scene>
</library_visual_scenes>
<scene>
<instance_visual_scene url="#Scene"/>
</scene>
</COLLADA>
+8
View File
@@ -0,0 +1,8 @@
MIT License
Copyright (c) 2019, Fan Fei
Permission is hereby granted, free of charge, to any person obtaining a copy of this software and associated documentation files (the ""Software""), to deal in the Software without restriction, including without limitation the rights to use, copy, modify, merge, publish, distribute, sublicense, and/or sell copies of the Software, and to permit persons to whom the Software is furnished to do so, subject to the following conditions:
The above copyright notice and this permission notice shall be included in all copies or substantial portions of the Software.
THE SOFTWARE IS PROVIDED *AS IS*, WITHOUT WARRANTY OF ANY KIND, EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE SOFTWARE.
@@ -0,0 +1,104 @@
[
{
"id": 0,
"name": "flapper_sc_nominal",
"urdf_file": "flappy/urdf/fwmav/flapper_sc_nominal.urdf",
"frequency": 34,
"wing_length": 0.07,
"mean_chord": 0.021212121212121,
"r33": 0.205833311654341,
"r22": 0.284203623407408,
"r11": 0.450820740740741,
"r00": 0.999407407407407,
"z_cp2": 0.246352600140835,
"z_cp1": 0.415846717980795,
"z_cp0": 1.028078968449933,
"z_rd": 1.174547978303502,
"left_shoulder_width": 13.95E-3,
"right_shoulder_width": 13.95E-3,
"stroke_plane_offset": 18.9913E-3,
"left_spring_stiffness": 0.013384289,
"right_spring_stiffness": 0.013384289,
"left_stroke_lower": -1.63,
"left_stroke_upper": 1.63,
"left_rotate_lower": -0.7854,
"left_rotate_upper": 0.7854,
"right_stroke_lower": -1.63,
"right_stroke_upper": 1.63,
"right_rotate_lower": -0.7854,
"right_rotate_upper": 0.7854,
"left_stroke_mid": 0.0,
"right_stroke_mid": 0.0,
"left_motor_properties":
{
"resistance": 12.4,
"torque_constant": 1.75e-3,
"gear_ratio": 10,
"mechanical_efficiency": 0.9,
"friction_coefficient": 2e-5,
"damping_coefficient": 9.74e-9,
"inertia": 7.03e-10
},
"right_motor_properties":
{
"resistance": 12.4,
"torque_constant": 1.75e-3,
"gear_ratio": 10,
"mechanical_efficiency": 0.9,
"friction_coefficient": 2e-5,
"damping_coefficient": 9.74e-9,
"inertia": 7.03e-10
}
},
{
"id": 1,
"name": "flapper_sc_trim",
"urdf_file": "flappy/urdf/fwmav/flapper_sc_nominal.urdf",
"frequency": 34,
"wing_length": 0.07,
"mean_chord": 0.021212121212121,
"r33": 0.205833311654341,
"r22": 0.284203623407408,
"r11": 0.450820740740741,
"r00": 0.999407407407407,
"z_cp2": 0.246352600140835,
"z_cp1": 0.415846717980795,
"z_cp0": 1.028078968449933,
"z_rd": 1.174547978303502,
"left_shoulder_width": 13.95E-3,
"right_shoulder_width": 13.95E-3,
"stroke_plane_offset": 18.9913E-3,
"left_spring_stiffness": 0.0133599752,
"right_spring_stiffness": 0.0133000000,
"left_stroke_lower": -1.63,
"left_stroke_upper": 1.63,
"left_rotate_lower": -0.844856704,
"left_rotate_upper": 0.765164977,
"right_stroke_lower": -1.63,
"right_stroke_upper": 1.63,
"right_rotate_lower": -0.854799666,
"right_rotate_upper": 0.814000120,
"left_stroke_mid": 0.0403463879,
"right_stroke_mid": 0.0319281979,
"left_motor_properties":
{
"resistance": 14.780065776,
"torque_constant": 1.75e-3,
"gear_ratio": 10,
"mechanical_efficiency": 0.9,
"friction_coefficient": 2e-5,
"damping_coefficient": 9.74e-9,
"inertia": 7.03e-10
},
"right_motor_properties":
{
"resistance": 13.763265084,
"torque_constant": 1.75e-3,
"gear_ratio": 10,
"mechanical_efficiency": 0.9,
"friction_coefficient": 2e-5,
"damping_coefficient": 9.74e-9,
"inertia": 7.03e-10
}
}
]
@@ -0,0 +1,9 @@
{
"f_sim" : 1e4,
"f_driver" : 1e3,
"f_sensor" : 500,
"f_control" : 500,
"f_imu" : 1000,
"f_vicon" : 200,
"f_visual" : 24
}
+186
View File
@@ -0,0 +1,186 @@
<?xml version="1.0" ?>
<!--********************** FWMAV Simulation *************************
# Version 0.3
# Fan Fei Feb 2019
# Direct motor driven flapping wing MAV simulation
********************************************************************-->
<robot name="flapper_sc">
<material name = "flapper/black">
<color rgba = "0 0 0 1"/>
</material>
<material name = "flapper/blue">
<color rgba = "0.0 0.0 1.0 1"/>
</material>
<material name = "flapper/red">
<color rgba = "1.0 0.0 0.0 1"/>
</material>
<!--link name = "world"/>
<joint name = "torso_to_world" type="floating">
<parent link = "world"/>
<child link = "torso"/>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
</joint-->
<link name = "torso">
<inertial>
<origin xyz = "0.1797E-3 0.0008E-3 -1.3998E-3" rpy = "0 0 0"/>
<mass value = "10.9067E-3"/>
<inertia
ixx = "4238.1285E-9"
iyy = "3970.1646E-9"
izz = "2440.9505E-9"
ixy = "-76.8896E-9"
iyz = "0.3011E-9"
ixz = "16.5500E-9"/>
</inertial>
<visual>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/torso_small_base.STL"/>
</geometry>
<material name = "flapper/black"/>
</visual>
<collision>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/torso_small_base.STL"/>
</geometry>
</collision>
</link>
<link name = "left_wing">
<inertial>
<origin xyz = "0.0024E-3 37.3242E-3 -9.8917E-3" rpy = "0 0 0"/>
<mass value = "0.0626E-3"/>
<inertia
ixx = "21.4402E-9"
iyy = "2.2204E-9"
izz = "19.2209E-9"
ixy = "-0.0000E-9"
iyz = "0.1968E-9"
ixz = "-0.0001E-9"/>
</inertial>
<visual>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/Wing_Camber_70mm_C35mm_no_trailing_L.STL"/>
</geometry>
<material name = "flapper/blue"/>
</visual>
<collision>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/Wing_Camber_70mm_C35mm_no_trailing_L.STL"/>
</geometry>
</collision>
</link>
<link name = "right_wing">
<inertial>
<origin xyz = "-0.0024E-3 -37.3242E-3 -9.8917E-3" rpy = "0 0 0"/>
<mass value = "0.0626E-3"/>
<inertia
ixx = "21.4402E-9"
iyy = "2.2204E-9"
izz = "19.2209E-9"
ixy = "-0.0000E-9"
iyz = "-0.1968E-9"
ixz = "0.0001E-9"/>
</inertial>
<visual>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/right_wing.STL"/>
</geometry>
<material name = "flapper/red"/>
</visual>
<collision>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/right_wing.STL"/>
</geometry>
</collision>
</link>
<link name="left_leading_edge">
<inertial>
<origin xyz = "-0.2837E-3 3.3023E-3 -6.3984E-3" rpy = "0 0 0"/>
<mass value = "0.7081E-3"/>
<inertia
ixx = "132.8411E-9"
iyy = "47.7258E-9"
izz = "90.6904E-9"
ixy = "-0.0416E-9"
iyz = "12.5149E-9"
ixz = "-0.4990E-9"/>
</inertial>
<visual>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/left_LE.STL"/>
</geometry>
<material name = "flapper/blue"/>
</visual>
</link>
<link name="right_leading_edge">
<inertial>
<origin xyz = "-0.2837E-3 -3.3023E-3 -6.3984E-3" rpy = "0 0 0"/>
<mass value = "0.7081E-3"/>
<inertia
ixx = "132.8411E-9"
iyy = "47.7258E-9"
izz = "90.6904E-9"
ixy = "0.0416E-9"
iyz = "-12.5149E-9"
ixz = "-0.4990E-9"/>
</inertial>
<visual>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<geometry>
<mesh filename = "meshes/right_LE.STL"/>
</geometry>
<material name = "flapper/red"/>
</visual>
</link>
<joint name = "left_stroke" type = "revolute">
<parent link = "torso"/>
<child link = "left_leading_edge"/>
<origin xyz = "0 13.95E-3 18.9913E-3" rpy = "0 0 0"/>
<axis xyz = "0 0 1"/>
<dynamics friction = "1E-9" damping = "8E-9"/>
<limit lower = "-1.63" upper = "1.63" effort = "0.02" velocity = "400"/>
</joint>
<joint name = "left_rotate" type = "revolute">
<parent link = "left_leading_edge"/>
<child link = "left_wing"/>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<axis xyz = "0 1 0"/>
<dynamics friction = "1E-8" damping = "1E-9"/>
<limit lower = "-0.7854" upper = "0.7854" effort = "0.02" velocity = "2000"/>
</joint>
<joint name = "right_stroke" type = "revolute">
<parent link = "torso"/>
<child link = "right_leading_edge"/>
<origin xyz = "0 -13.95E-3 18.9913E-3" rpy = "0 0 0"/>
<axis xyz = "0 0 -1"/>
<dynamics friction = "1E-9" damping = "8E-9"/>
<limit lower = "-1.63" upper = "1.63" effort = "0.02" velocity = "400"/>
</joint>
<joint name = "right_rotate" type = "revolute">
<parent link = "right_leading_edge"/>
<child link = "right_wing"/>
<origin xyz = "0 0 0" rpy = "0 0 0"/>
<axis xyz = "0 1 0"/>
<dynamics friction = "1E-8" damping = "1E-9"/>
<limit lower = "-0.7854" upper = "0.7854" effort = "0.02" velocity = "2000"/>
</joint>
</robot>
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+176
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+63
View File
@@ -0,0 +1,63 @@
<?xml version="1.0" encoding="UTF-8"?>
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</mesh>
</geometry>
</library_geometries>
<library_controllers/>
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<node id="Camera" name="Camera" type="NODE">
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<instance_camera url="#Camera-camera"/>
</node>
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<instance_light url="#Lamp-light"/>
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<instance_geometry url="#Left_Aileron-mesh"/>
</node>
</visual_scene>
</library_visual_scenes>
<scene>
<instance_visual_scene url="#Scene"/>
</scene>
</COLLADA>
@@ -0,0 +1,167 @@
<?xml version="1.0" encoding="utf-8"?>
<COLLADA xmlns="http://www.collada.org/2005/11/COLLADASchema" version="1.4.1">
<asset>
<contributor>
<author>Original CAD work - Wayne Garris</author>
</contributor>
<contributor>
<author>Pavel Vechersky</author>
<authoring_tool>Blender 2.71.0 commit date:2014-06-12, commit time:18:39, hash:169c95b</authoring_tool>
</contributor>
<created>2016-07-12T18:21:31</created>
<modified>2016-07-12T18:21:31</modified>
<unit name="meter" meter="1"/>
<up_axis>Z_UP</up_axis>
</asset>
<library_cameras>
<camera id="Camera-camera" name="Camera">
<optics>
<technique_common>
<perspective>
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<zfar sid="zfar">100</zfar>
</perspective>
</technique_common>
</optics>
<extra>
<technique profile="blender">
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<shiftx>0</shiftx>
<shifty>0</shifty>
</technique>
</extra>
</camera>
</library_cameras>
<library_lights>
<light id="Lamp-light" name="Lamp">
<technique_common>
<point>
<color sid="color">1 1 1</color>
<constant_attenuation>1</constant_attenuation>
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</technique_common>
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<area_sizey>0.1</area_sizey>
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<att1>0</att1>
<att2>1</att2>
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<red>1</red>
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<skyblendfac>1</skyblendfac>
<skyblendtype>1</skyblendtype>
<soft>3</soft>
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<sun_brightness>1</sun_brightness>
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<sun_intensity>1</sun_intensity>
<sun_size>1</sun_size>
<type>0</type>
</technique>
</extra>
</light>
</library_lights>
<library_images/>
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@@ -0,0 +1,163 @@
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<param name="X" type="float"/>
<param name="Y" type="float"/>
<param name="Z" type="float"/>
</accessor>
</technique_common>
</source>
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<library_controllers/>
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<instance_camera url="#Camera-camera"/>
</node>
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<instance_light url="#Lamp-light"/>
</node>
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<instance_geometry url="#Rudder-mesh"/>
</node>
</visual_scene>
</library_visual_scenes>
<scene>
<instance_visual_scene url="#Scene"/>
</scene>
</COLLADA>
+303
View File
@@ -0,0 +1,303 @@
<?xml version="1.0" ?>
<!-- =================================================================================== -->
<!-- | This document was autogenerated by xacro from techpod.xacro | -->
<!-- | EDITING THIS FILE BY HAND IS NOT RECOMMENDED | -->
<!-- =================================================================================== -->
<!--
Copyright 2016 Pavel Vechersky, ASL, ETH Zurich, Switzerland
Licensed under the Apache License, Version 2.0 (the "License");
you may not use this file except in compliance with the License.
You may obtain a copy of the License at
http://www.apache.org/licenses/LICENSE-2.0
Unless required by applicable law or agreed to in writing, software
distributed under the License is distributed on an "AS IS" BASIS,
WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
See the License for the specific language governing permissions and
limitations under the License.
-->
<robot name="techpod" xmlns:xacro="http://ros.org/wiki/xacro">
<material name="black">
<color rgba="0.2 0.2 0.2 1"/>
</material>
<material name="white">
<color rgba="0.9 0.9 0.9 1"/>
</material>
<material name="dark_gray">
<color rgba="0.3 0.3 0.3 1"/>
</material>
<material name="gray">
<color rgba="0.5 0.5 0.5 1"/>
</material>
<material name="light_gray">
<color rgba="0.7 0.7 0.7 1"/>
</material>
<material name="pure_red">
<color rgba="1.0 0.0 0.0 1"/>
</material>
<material name="red">
<color rgba="0.8 0.1 0.1 1"/>
</material>
<material name="pure_green">
<color rgba="0.0 1.0 0.0 1"/>
</material>
<material name="pure_blue">
<color rgba="0.0 0.0 1.0 1"/>
</material>
<material name="blue">
<color rgba="0.0 0.2 0.8 1"/>
</material>
<!-- [kg] -->
<link name="ns/base_link">
<inertial>
<origin rpy="0 0 0" xyz="0 0 0"/>
<mass value="1e-6"/>
<inertia ixx="1e-12" ixy="0.0" ixz="0.0" iyy="1e-12" iyz="0.0" izz="1e-12"/>
</inertial>
</link> <!-- in pybullet, the inertia need to be specified even for dummy links, otherwise it will put an identity inertia and a mass of 1 by default -->
<joint name="ns/base_joint" type="fixed">
<origin rpy="0 0 0" xyz="0 0 0"/>
<parent link="ns/base_link"/>
<child link="ns/base_link_inertia"/>
</joint>
<link name="ns/base_link_inertia">
<inertial>
<mass value="2.05"/>
<origin rpy="0 0 0" xyz="0 0 0"/>
<inertia ixx="0.16632" ixy="0.0" ixz="0.0755" iyy="0.3899" iyz="0.0" izz="0.5243"/>
</inertial>
<visual>
<material name="white"/>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_body.dae" scale="1 1 1"/>
</geometry>
</visual>
<collision>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<box size="1.088 2.591 0.303"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/base_link">
<material>Gazebo/Gray</material>
</gazebo>
<!-- Attach fw_dynamics to the base_link -->
<gazebo>
<plugin filename="librotors_gazebo_fw_dynamics_plugin.so" name="fw_dynamics_plugin">
<robotNamespace>ns</robotNamespace>
<linkName>ns/base_link</linkName>
<aeroParamsYAML>aero_params</aeroParamsYAML>
<vehicleParamsYAML>vehicle_params</vehicleParamsYAML>
<isInputJoystick>true</isInputJoystick>
</plugin>
</gazebo>
<joint name="ns/aileron_left_joint" type="revolute">
<origin rpy="0 0 0" xyz="0.1095 0.99245 0.115"/>
<axis xyz="0 -1 0"/>
<parent link="ns/base_link"/>
<child link="ns/aileron_left"/>
<limit effort="0" lower="0" upper="0" velocity="0"/>
</joint>
<link name="ns/aileron_left">
<inertial>
<origin rpy="0 0 0" xyz="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.0010164162601" ixy="0.0" ixz="0.0" iyy="2.481665674e-05" iyz="0.0" izz="0.0010384162513"/>
</inertial>
<visual>
<material name="red"/>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_aileron_left.dae" scale="1 1 1"/>
</geometry>
</visual>
<collision>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_aileron_left.dae" scale="1 1 1"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/aileron_left">
<material>Gazebo/Red</material>
</gazebo>
<joint name="ns/aileron_right_joint" type="revolute">
<origin rpy="0 0 0" xyz="0.1095 -0.99245 0.115"/>
<axis xyz="0 1 0"/>
<parent link="ns/base_link"/>
<child link="ns/aileron_right"/>
<limit effort="0" lower="0" upper="0" velocity="0"/>
</joint>
<link name="ns/aileron_right">
<inertial>
<origin rpy="0 0 0" xyz="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.0010164162601" ixy="0.0" ixz="0.0" iyy="2.481665674e-05" iyz="0.0" izz="0.0010384162513"/>
</inertial>
<visual>
<material name="blue"/>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_aileron_right.dae" scale="1 1 1"/>
</geometry>
</visual>
<collision>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_aileron_right.dae" scale="1 1 1"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/aileron_right">
<material>Gazebo/Red</material>
</gazebo>
<joint name="ns/elevator_joint" type="revolute">
<origin rpy="0 0 0" xyz="-0.555 0 0.26"/>
<axis xyz="0 -1 0"/>
<parent link="ns/base_link"/>
<child link="ns/elevator"/>
<limit effort="0" lower="0" upper="0" velocity="0"/>
</joint>
<link name="ns/elevator">
<inertial>
<origin rpy="0 0 0" xyz="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.00174160763669" ixy="0.0" ixz="0.0" iyy="2.287499085e-05" iyz="0.0" izz="0.0017620826285"/>
</inertial>
<visual>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_elevator.dae" scale="1 1 1"/>
</geometry>
</visual>
<collision>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_elevator.dae" scale="1 1 1"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/elevator">
<material>Gazebo/Blue</material>
</gazebo>
<joint name="ns/flap_left_joint" type="revolute">
<origin rpy="0 0 0" xyz="0.101 0.382 0.1185"/>
<axis xyz="0 -1 0"/>
<parent link="ns/base_link"/>
<child link="ns/flap_left"/>
<limit effort="0" lower="0" upper="0" velocity="0"/>
</joint>
<link name="ns/flap_left">
<inertial>
<origin rpy="0 0 0" xyz="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.00175780763021" ixy="0.0" ixz="0.0" iyy="5.026664656e-05" iyz="0.0" izz="0.00180380761181"/>
</inertial>
<visual>
<material name="red"/>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_flap_left.dae" scale="1 1 1"/>
</geometry>
</visual>
<collision>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_flap_left.dae" scale="1 1 1"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/flap_left">
<material>Gazebo/Yellow</material>
</gazebo>
<joint name="ns/flap_right_joint" type="revolute">
<origin rpy="0 0 0" xyz="0.101 -0.382 0.1185"/>
<axis xyz="0 1 0"/>
<parent link="ns/base_link"/>
<child link="ns/flap_right"/>
<limit effort="0" lower="0" upper="0" velocity="0"/>
</joint>
<link name="ns/flap_right">
<inertial>
<origin rpy="0 0 0" xyz="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.00175780763021" ixy="0.0" ixz="0.0" iyy="5.026664656e-05" iyz="0.0" izz="0.00180380761181"/>
</inertial>
<visual>
<material name="blue"/>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_flap_right.dae" scale="1 1 1"/>
</geometry>
</visual>
<collision>
<origin rpy="0 0 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_flap_right.dae" scale="1 1 1"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/flap_right">
<material>Gazebo/Yellow</material>
</gazebo>
<joint name="ns/rudder_joint" type="revolute">
<origin rpy="0 -0.25 0" xyz="-0.428 0 0"/>
<axis xyz="0 0 1"/>
<parent link="ns/base_link"/>
<child link="ns/rudder"/>
<limit effort="0" lower="0" upper="0" velocity="0"/>
</joint>
<link name="ns/rudder">
<inertial>
<origin rpy="0 0.25 0" xyz="0 0 0"/>
<mass value="0.1"/>
<inertia ixx="0.00048670813865" ixy="0.0" ixz="0.0" iyy="0.00062268308426" iyz="0.0" izz="0.00014137494345"/>
</inertial>
<visual>
<origin rpy="0 0.25 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_rudder.dae" scale="1 1 1"/>
</geometry>
</visual>
<collision>
<origin rpy="0 0.25 0" xyz="0 0 0"/>
<geometry>
<mesh filename="meshes/techpod/techpod_rudder.dae" scale="1 1 1"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/rudder">
<material>Gazebo/Orange</material>
</gazebo>
<joint name="ns/propeller_{suffix}_joint" type="continuous">
<origin rpy="0 -1.57079632679 0" xyz="-0.025 0 0.15"/>
<axis xyz="0 0 1"/>
<parent link="ns/base_link"/>
<child link="ns/propeller_"/>
</joint>
<link name="ns/propeller_">
<inertial>
<mass value="0.1"/>
<inertia ixx="0.0025007489997" ixy="0.0" ixz="0.0" iyy="0.0025007489997" iyz="0.0" izz="0.005"/>
</inertial>
<visual>
<geometry>
<mesh filename="meshes/propeller_cw.dae" scale="0.1 0.1 0.1"/>
</geometry>
</visual>
<collision>
<geometry>
<mesh filename="meshes/propeller_cw.dae" scale="0.1 0.1 0.1"/>
</geometry>
</collision>
</link>
<gazebo reference="ns/propeller_">
<material>Gazebo/Gray</material>
</gazebo>
</robot>
+3 -2
View File
@@ -1389,7 +1389,8 @@ class Bullet(Simulator):
position = self.get_link_state(body_id, link_id)[0]
else: # local frame
position = (0., 0., 0.)
self.sim.applyExternalForce(body_id, link_id, force, position, frame)
self.sim.applyExternalForce(objectUniqueId=body_id, linkIndex=link_id, forceObj=force, posObj=position,
flags=frame)
def apply_external_torque(self, body_id, link_id=-1, torque=(0., 0., 0.), frame=Simulator.LINK_FRAME):
"""
@@ -1405,7 +1406,7 @@ class Bullet(Simulator):
frame (int): Specify the coordinate system of force/position: either `pybullet.WORLD_FRAME` (=2) for
Cartesian world coordinates or `pybullet.LINK_FRAME` (=1) for local link coordinates.
"""
self.sim.applyExternalTorque(body_id, link_id, torque)
self.sim.applyExternalTorque(objectUniqueId=body_id, linkIndex=link_id, torqueObj=torque, flags=frame)
###################
# transformations #