forked from USC-ACTLab/crazyswarm
-
Notifications
You must be signed in to change notification settings - Fork 62
Commit
This commit does not belong to any branch on this repository, and may belong to a fork outside of the repository.
Merge pull request #160 from IMRCLab/feature_sim_controller
Add physics-based simulation
- Loading branch information
Showing
9 changed files
with
599 additions
and
103 deletions.
There are no files selected for viewing
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -0,0 +1,125 @@ | ||
from __future__ import annotations | ||
|
||
from rclpy.node import Node | ||
from rosgraph_msgs.msg import Clock | ||
from rclpy.time import Time | ||
from ..sim_data_types import State, Action | ||
|
||
|
||
import numpy as np | ||
import rowan | ||
|
||
class Backend: | ||
"""Backend that uses newton-euler rigid-body dynamics implemented in numpy""" | ||
|
||
def __init__(self, node: Node, names: list[str], states: list[State]): | ||
self.node = node | ||
self.names = names | ||
self.clock_publisher = node.create_publisher(Clock, 'clock', 10) | ||
self.t = 0 | ||
self.dt = 0.0005 | ||
|
||
self.uavs = [] | ||
for state in states: | ||
uav = Quadrotor(state) | ||
self.uavs.append(uav) | ||
|
||
def time(self) -> float: | ||
return self.t | ||
|
||
def step(self, states_desired: list[State], actions: list[Action]) -> list[State]: | ||
# advance the time | ||
self.t += self.dt | ||
|
||
next_states = [] | ||
|
||
for uav, action in zip(self.uavs, actions): | ||
uav.step(action, self.dt) | ||
next_states.append(uav.state) | ||
|
||
# print(states_desired, actions, next_states) | ||
# publish the current clock | ||
clock_message = Clock() | ||
clock_message.clock = Time(seconds=self.time()).to_msg() | ||
self.clock_publisher.publish(clock_message) | ||
|
||
return next_states | ||
|
||
def shutdown(self): | ||
pass | ||
|
||
|
||
class Quadrotor: | ||
"""Basic rigid body quadrotor model (no drag) using numpy and rowan""" | ||
|
||
def __init__(self, state): | ||
# parameters (Crazyflie 2.0 quadrotor) | ||
self.mass = 0.034 # kg | ||
# self.J = np.array([ | ||
# [16.56,0.83,0.71], | ||
# [0.83,16.66,1.8], | ||
# [0.72,1.8,29.26] | ||
# ]) * 1e-6 # kg m^2 | ||
self.J = np.array([16.571710e-6, 16.655602e-6, 29.261652e-6]) | ||
|
||
# Note: we assume here that our control is forces | ||
arm_length = 0.046 # m | ||
arm = 0.707106781 * arm_length | ||
t2t = 0.006 # thrust-to-torque ratio | ||
self.B0 = np.array([ | ||
[1, 1, 1, 1], | ||
[-arm, -arm, arm, arm], | ||
[-arm, arm, arm, -arm], | ||
[-t2t, t2t, -t2t, t2t] | ||
]) | ||
self.g = 9.81 # not signed | ||
|
||
if self.J.shape == (3,3): | ||
self.inv_J = np.linalg.pinv(self.J) # full matrix -> pseudo inverse | ||
else: | ||
self.inv_J = 1 / self.J # diagonal matrix -> division | ||
|
||
self.state = state | ||
|
||
def step(self, action, dt): | ||
|
||
# convert RPM -> Force | ||
def rpm_to_force(rpm): | ||
# polyfit using Tobias' data | ||
p = [2.55077341e-08, -4.92422570e-05, -1.51910248e-01] | ||
force_in_grams = np.polyval(p, rpm) | ||
force_in_newton = force_in_grams * 9.81 / 1000.0 | ||
return np.maximum(force_in_newton, 0) | ||
|
||
force = rpm_to_force(action.rpm) | ||
|
||
# compute next state | ||
eta = np.dot(self.B0, force) | ||
f_u = np.array([0,0,eta[0]]) | ||
tau_u = np.array([eta[1],eta[2],eta[3]]) | ||
|
||
# dynamics | ||
# dot{p} = v | ||
pos_next = self.state.pos + self.state.vel * dt | ||
# mv = mg + R f_u | ||
vel_next = self.state.vel + (np.array([0,0,-self.g]) + rowan.rotate(self.state.quat,f_u) / self.mass) * dt | ||
|
||
# dot{R} = R S(w) | ||
# to integrate the dynamics, see | ||
# https://www.ashwinnarayan.com/post/how-to-integrate-quaternions/, and | ||
# https://arxiv.org/pdf/1604.08139.pdf | ||
q_next = rowan.normalize(rowan.calculus.integrate(self.state.quat, self.state.omega, dt)) | ||
|
||
# mJ = Jw x w + tau_u | ||
omega_next = self.state.omega + (self.inv_J * (np.cross(self.J * self.state.omega, self.state.omega) + tau_u)) * dt | ||
|
||
self.state.pos = pos_next | ||
self.state.vel = vel_next | ||
self.state.quat = q_next | ||
self.state.omega = omega_next | ||
|
||
# if we fall below the ground, set velocities to 0 | ||
if self.state.pos[2] < 0: | ||
self.state.pos[2] = 0 | ||
self.state.vel = [0,0,0] | ||
self.state.omega = [0,0,0] |
This file contains bidirectional Unicode text that may be interpreted or compiled differently than what appears below. To review, open the file in an editor that reveals hidden Unicode characters.
Learn more about bidirectional Unicode characters
Oops, something went wrong.