mirror of
https://github.com/bulletphysics/bullet3.git
synced 2026-09-10 20:38:26 +00:00
148 lines
5.1 KiB
Python
148 lines
5.1 KiB
Python
import numpy as np
|
|
|
|
|
|
class PDControllerStableMultiDof(object):
|
|
|
|
def __init__(self, pb):
|
|
self._pb = pb
|
|
|
|
def computePD(self, bodyUniqueId, jointIndices, desiredPositions, desiredVelocities, kps, kds,
|
|
maxForces, timeStep):
|
|
|
|
numJoints = len(jointIndices) #self._pb.getNumJoints(bodyUniqueId)
|
|
curPos, curOrn = self._pb.getBasePositionAndOrientation(bodyUniqueId)
|
|
#q1 = [desiredPositions[0],desiredPositions[1],desiredPositions[2],desiredPositions[3],desiredPositions[4],desiredPositions[5],desiredPositions[6]]
|
|
q1 = [curPos[0], curPos[1], curPos[2], curOrn[0], curOrn[1], curOrn[2], curOrn[3]]
|
|
|
|
#qdot1 = [0,0,0, 0,0,0,0]
|
|
baseLinVel, baseAngVel = self._pb.getBaseVelocity(bodyUniqueId)
|
|
|
|
qdot1 = [
|
|
baseLinVel[0], baseLinVel[1], baseLinVel[2], baseAngVel[0], baseAngVel[1], baseAngVel[2], 0
|
|
]
|
|
qError = [0, 0, 0, 0, 0, 0, 0]
|
|
|
|
qIndex = 7
|
|
qdotIndex = 7
|
|
zeroAccelerations = [0, 0, 0, 0, 0, 0, 0]
|
|
for i in range(numJoints):
|
|
js = self._pb.getJointStateMultiDof(bodyUniqueId, jointIndices[i])
|
|
|
|
jointPos = js[0]
|
|
jointVel = js[1]
|
|
q1 += jointPos
|
|
|
|
if len(js[0]) == 1:
|
|
desiredPos = desiredPositions[qIndex]
|
|
|
|
qdiff = desiredPos - jointPos[0]
|
|
qError.append(qdiff)
|
|
zeroAccelerations.append(0.)
|
|
qdot1 += jointVel
|
|
qIndex += 1
|
|
qdotIndex += 1
|
|
if len(js[0]) == 4:
|
|
desiredPos = [
|
|
desiredPositions[qIndex], desiredPositions[qIndex + 1], desiredPositions[qIndex + 2],
|
|
desiredPositions[qIndex + 3]
|
|
]
|
|
axis = self._pb.getAxisDifferenceQuaternion(desiredPos, jointPos)
|
|
jointVelNew = [jointVel[0], jointVel[1], jointVel[2], 0]
|
|
qdot1 += jointVelNew
|
|
qError.append(axis[0])
|
|
qError.append(axis[1])
|
|
qError.append(axis[2])
|
|
qError.append(0)
|
|
desiredVel = [
|
|
desiredVelocities[qdotIndex], desiredVelocities[qdotIndex + 1],
|
|
desiredVelocities[qdotIndex + 2]
|
|
]
|
|
zeroAccelerations += [0., 0., 0., 0.]
|
|
qIndex += 4
|
|
qdotIndex += 4
|
|
|
|
q = np.array(q1)
|
|
qdot = np.array(qdot1)
|
|
|
|
qdotdesired = np.array(desiredVelocities)
|
|
qdoterr = qdotdesired - qdot
|
|
|
|
Kp = np.diagflat(kps)
|
|
Kd = np.diagflat(kds)
|
|
|
|
# Compute -Kp(q + qdot - qdes)
|
|
p_term = Kp.dot(qError - qdot*timeStep)
|
|
# Compute -Kd(qdot - qdotdes)
|
|
d_term = Kd.dot(qdoterr)
|
|
|
|
# Compute Inertia matrix M(q)
|
|
M = self._pb.calculateMassMatrix(bodyUniqueId, q1, flags=1)
|
|
M = np.array(M)
|
|
# Given: M(q) * qddot + C(q, qdot) = T_ext + T_int
|
|
# Compute Coriolis and External (Gravitational) terms G = C - T_ext
|
|
G = self._pb.calculateInverseDynamics(bodyUniqueId, q1, qdot1, zeroAccelerations, flags=1)
|
|
G = np.array(G)
|
|
# Obtain estimated generalized accelerations, considering Coriolis and Gravitational forces, and stable PD actions
|
|
qddot = np.linalg.solve(a=(M + Kd * timeStep),
|
|
b=p_term + d_term - G)
|
|
# Compute control generalized forces (T_int)
|
|
tau = p_term + d_term - Kd.dot(qddot) * timeStep
|
|
# Clip generalized forces to actuator limits
|
|
maxF = np.array(maxForces)
|
|
generalized_forces = np.clip(tau, -maxF, maxF)
|
|
return generalized_forces
|
|
|
|
|
|
class PDControllerStable(object):
|
|
"""
|
|
Implementation based on: Tan, J., Liu, K., & Turk, G. (2011). "Stable proportional-derivative controllers"
|
|
DOI: 10.1109/MCG.2011.30
|
|
"""
|
|
def __init__(self, pb):
|
|
self._pb = pb
|
|
|
|
def computePD(self, bodyUniqueId, jointIndices, desiredPositions, desiredVelocities, kps, kds,
|
|
maxForces, timeStep):
|
|
numJoints = self._pb.getNumJoints(bodyUniqueId)
|
|
jointStates = self._pb.getJointStates(bodyUniqueId, jointIndices)
|
|
q1 = []
|
|
qdot1 = []
|
|
zeroAccelerations = []
|
|
for i in range(numJoints):
|
|
q1.append(jointStates[i][0])
|
|
qdot1.append(jointStates[i][1])
|
|
zeroAccelerations.append(0)
|
|
|
|
q = np.array(q1)
|
|
qdot = np.array(qdot1)
|
|
qdes = np.array(desiredPositions)
|
|
qdotdes = np.array(desiredVelocities)
|
|
|
|
qError = qdes - q
|
|
qdotError = qdotdes - qdot
|
|
|
|
Kp = np.diagflat(kps)
|
|
Kd = np.diagflat(kds)
|
|
|
|
# Compute -Kp(q + qdot - qdes)
|
|
p_term = Kp.dot(qError - qdot*timeStep)
|
|
# Compute -Kd(qdot - qdotdes)
|
|
d_term = Kd.dot(qdotError)
|
|
|
|
# Compute Inertia matrix M(q)
|
|
M = self._pb.calculateMassMatrix(bodyUniqueId, q1)
|
|
M = np.array(M)
|
|
# Given: M(q) * qddot + C(q, qdot) = T_ext + T_int
|
|
# Compute Coriolis and External (Gravitational) terms G = C - T_ext
|
|
G = self._pb.calculateInverseDynamics(bodyUniqueId, q1, qdot1, zeroAccelerations)
|
|
G = np.array(G)
|
|
# Obtain estimated generalized accelerations, considering Coriolis and Gravitational forces, and stable PD actions
|
|
qddot = np.linalg.solve(a=(M + Kd * timeStep),
|
|
b=(-G + p_term + d_term))
|
|
# Compute control generalized forces (T_int)
|
|
tau = p_term + d_term - (Kd.dot(qddot) * timeStep)
|
|
# Clip generalized forces to actuator limits
|
|
maxF = np.array(maxForces)
|
|
generalized_forces = np.clip(tau, -maxF, maxF)
|
|
return generalized_forces
|