Merge pull request AtsushiSakai#98 from daniel-s-ingram/master

Close AtsushiSakai#98 Quadrotor simulation

Author: AtsushiSakai

AerialNavigation/Quadrotor.py

@@ -0,0 +1,79 @@
+"""
+Class for plotting a quadrotor
+
+Author: Daniel Ingram (daniel-s-ingram)
+"""
+
+from math import cos, sin
+import numpy as np
+import matplotlib.pyplot as plt
+from mpl_toolkits.mplot3d import Axes3D
+
+class Quadrotor():
+    def __init__(self, x=0, y=0, z=0, roll=0, pitch=0, yaw=0, size=0.25):
+        self.p1 = np.array([size/2, 0, 0, 1]).T
+        self.p2 = np.array([-size/2, 0, 0, 1]).T
+        self.p3 = np.array([0, size/2, 0, 1]).T
+        self.p4 = np.array([0, -size/2, 0, 1]).T
+
+        self.x_data = []
+        self.y_data = []
+        self.z_data = []
+
+        plt.ion()
+
+        fig = plt.figure()
+        self.ax = fig.add_subplot(111, projection='3d')
+
+        self.update_pose(x, y, z, roll, pitch, yaw)
+
+    def update_pose(self, x, y, z, roll, pitch, yaw):
+        self.x = x
+        self.y = y
+        self.z = z
+        self.roll = roll
+        self.pitch = pitch
+        self.yaw = yaw
+        self.x_data.append(x)
+        self.y_data.append(y)
+        self.z_data.append(z)
+        self.plot()
+
+    def transformation_matrix(self):
+        x = self.x
+        y = self.y
+        z = self.z
+        roll = self.roll
+        pitch = self.pitch
+        yaw = self.yaw
+        return np.array(
+            [[cos(yaw)*cos(pitch), -sin(yaw)*cos(roll)+cos(yaw)*sin(pitch)*sin(roll), sin(yaw)*sin(roll)+cos(yaw)*sin(pitch)*cos(roll), x],
+             [sin(yaw)*cos(pitch), cos(yaw)*cos(roll)+sin(yaw)*sin(pitch)*sin(roll), -cos(yaw)*sin(roll)+sin(yaw)*sin(pitch)*cos(roll), y],
+             [-sin(pitch), cos(pitch)*sin(roll), cos(pitch)*cos(yaw), z]
+            ])
+
+    def plot(self):
+        T = self.transformation_matrix()
+
+        p1_t = np.matmul(T, self.p1)
+        p2_t = np.matmul(T, self.p2)
+        p3_t = np.matmul(T, self.p3)
+        p4_t = np.matmul(T, self.p4)
+
+        plt.cla()
+
+        self.ax.plot([p1_t[0], p2_t[0], p3_t[0], p4_t[0]],
+                     [p1_t[1], p2_t[1], p3_t[1], p4_t[1]],
+                     [p1_t[2], p2_t[2], p3_t[2], p4_t[2]], 'k.')
+
+        self.ax.plot([p1_t[0], p2_t[0]], [p1_t[1], p2_t[1]], [p1_t[2], p2_t[2]], 'r-')
+        self.ax.plot([p3_t[0], p4_t[0]], [p3_t[1], p4_t[1]], [p3_t[2], p4_t[2]], 'r-')
+
+        self.ax.plot(self.x_data, self.y_data, self.z_data, 'b:')
+
+        plt.xlim(-5, 5)
+        plt.ylim(-5, 5)
+        self.ax.set_zlim(0, 10)
+
+        plt.show()
+        plt.pause(0.001)

AerialNavigation/TrajectoryGenerator.py

@@ -0,0 +1,76 @@
+"""
+Generates a quintic polynomial trajectory.
+
+Author: Daniel Ingram (daniel-s-ingram)
+"""
+
+import numpy as np
+
+class TrajectoryGenerator():
+    def __init__(self, start_pos, des_pos, T, start_vel=[0,0,0], des_vel=[0,0,0], start_acc=[0,0,0], des_acc=[0,0,0]):
+        self.start_x = start_pos[0]
+        self.start_y = start_pos[1]
+        self.start_z = start_pos[2]
+
+        self.des_x = des_pos[0]
+        self.des_y = des_pos[1]
+        self.des_z = des_pos[2]
+
+        self.start_x_vel = start_vel[0]
+        self.start_y_vel = start_vel[1]
+        self.start_z_vel = start_vel[2]
+
+        self.des_x_vel = des_vel[0]
+        self.des_y_vel = des_vel[1]
+        self.des_z_vel = des_vel[2]
+
+        self.start_x_acc = start_acc[0]
+        self.start_y_acc = start_acc[1]
+        self.start_z_acc = start_acc[2]
+
+        self.des_x_acc = des_acc[0]
+        self.des_y_acc = des_acc[1]
+        self.des_z_acc = des_acc[2]
+
+        self.T = T
+
+    def solve(self):
+        A = np.array(
+            [[0, 0, 0, 0, 0, 1],
+             [self.T**5, self.T**4, self.T**3, self.T**2, self.T, 1],
+             [0, 0, 0, 0, 1, 0],
+             [5*self.T**4, 4*self.T**3, 3*self.T**2, 2*self.T, 1, 0],
+             [0, 0, 0, 2, 0, 0],
+             [20*self.T**3, 12*self.T**2, 6*self.T, 2, 0, 0]
+            ])
+
+        b_x = np.array(
+            [[self.start_x],
+             [self.des_x],
+             [self.start_x_vel],
+             [self.des_x_vel],
+             [self.start_x_acc],
+             [self.des_x_acc]
+            ])
+
+        b_y = np.array(
+            [[self.start_y],
+             [self.des_y],
+             [self.start_y_vel],
+             [self.des_y_vel],
+             [self.start_y_acc],
+             [self.des_y_acc]
+            ])
+
+        b_z = np.array(
+            [[self.start_z],
+             [self.des_z],
+             [self.start_z_vel],
+             [self.des_z_vel],
+             [self.start_z_acc],
+             [self.des_z_acc]
+            ])
+
+        self.x_c = np.linalg.solve(A, b_x)
+        self.y_c = np.linalg.solve(A, b_y)
+        self.z_c = np.linalg.solve(A, b_z)

AerialNavigation/quad_sim.py

@@ -0,0 +1,189 @@
+"""
+Simulate a quadrotor following a 3D trajectory
+
+Author: Daniel Ingram (daniel-s-ingram)
+"""
+
+from math import cos, sin
+import numpy as np
+from Quadrotor import Quadrotor
+from TrajectoryGenerator import TrajectoryGenerator
+
+#Simulation parameters
+g = 9.81
+m = 0.2
+Ixx = 1
+Iyy = 1
+Izz = 1
+T = 5
+
+#Proportional coefficients
+Kp_x = 1
+Kp_y = 1
+Kp_z = 1
+Kp_roll = 25
+Kp_pitch = 25
+Kp_yaw = 25
+
+#Derivative coefficients
+Kd_x = 10
+Kd_y = 10
+Kd_z = 1
+
+def quad_sim(x_c, y_c, z_c):
+    """
+    Calculates the necessary thrust and torques for the quadrotor to
+    follow the trajectory described by the sets of coefficients
+    x_c, y_c, and z_c.
+    """
+    x_pos = -5
+    y_pos = -5
+    z_pos = 5
+    x_vel = 0
+    y_vel = 0
+    z_vel = 0
+    x_acc = 0
+    y_acc = 0
+    z_acc = 0
+    roll = 0
+    pitch = 0
+    yaw = 0
+    roll_vel = 0
+    pitch_vel = 0
+    yaw_vel = 0
+
+    des_yaw = 0
+
+    dt = 0.1
+    t = 0
+
+    q = Quadrotor(x=x_pos, y=y_pos, z=z_pos, roll=roll, pitch=pitch, yaw=yaw, size=1)
+
+    i = 0
+
+    while True:
+        while t <= T:
+            des_x_pos = calculate_position(x_c[i], t)
+            des_y_pos = calculate_position(y_c[i], t)
+            des_z_pos = calculate_position(z_c[i], t)
+            des_x_vel = calculate_velocity(x_c[i], t)
+            des_y_vel = calculate_velocity(y_c[i], t)
+            des_z_vel = calculate_velocity(z_c[i], t)
+            des_x_acc = calculate_acceleration(x_c[i], t)
+            des_y_acc = calculate_acceleration(y_c[i], t)
+            des_z_acc = calculate_acceleration(z_c[i], t)
+
+            thrust = m*(g + des_z_acc + Kp_z*(des_z_pos - z_pos) + Kd_z*(des_z_vel - z_vel))
+
+            roll_torque = Kp_roll*(((des_x_acc*sin(des_yaw) - des_y_acc*cos(des_yaw))/g) - roll)
+            pitch_torque = Kp_pitch*(((des_x_acc*cos(des_yaw) - des_y_acc*sin(des_yaw))/g) - pitch)
+            yaw_torque = Kp_yaw*(des_yaw - yaw)
+
+            roll_vel += roll_torque*dt/Ixx
+            pitch_vel += pitch_torque*dt/Iyy
+            yaw_vel += yaw_torque*dt/Izz
+
+            roll += roll_vel*dt
+            pitch += pitch_vel*dt
+            yaw += yaw_vel*dt
+
+            R = rotation_matrix(roll, pitch, yaw)
+            acc = (np.matmul(R, np.array([0, 0, thrust]).T) - np.array([0, 0, m*g]).T)/m
+            x_acc = acc[0]
+            y_acc = acc[1]
+            z_acc = acc[2]
+            x_vel += x_acc*dt
+            y_vel += y_acc*dt
+            z_vel += z_acc*dt
+            x_pos += x_vel*dt
+            y_pos += y_vel*dt
+            z_pos += z_vel*dt
+
+            q.update_pose(x_pos, y_pos, z_pos, roll, pitch, yaw)
+
+            t += dt
+
+        t = 0
+        i = (i+1)%4
+
+def calculate_position(c, t):
+    """
+    Calculates a position given a set of quintic coefficients and a time.
+
+    Args
+        c: List of coefficients generated by a quintic polynomial 
+            trajectory generator.
+        t: Time at which to calculate the position
+
+    Returns
+        Position
+    """
+    return c[0]*t**5 + c[1]*t**4 + c[2]*t**3 + c[3]*t**2 + c[4]*t + c[5]
+
+def calculate_velocity(c, t):
+    """
+    Calculates a velocity given a set of quintic coefficients and a time.
+
+    Args
+        c: List of coefficients generated by a quintic polynomial 
+            trajectory generator.
+        t: Time at which to calculate the velocity
+
+    Returns
+        Velocity
+    """
+    return 5*c[0]*t**4 + 4*c[1]*t**3 + 3*c[2]*t**2 + 2*c[3]*t + c[4]
+
+def calculate_acceleration(c, t):
+    """
+    Calculates an acceleration given a set of quintic coefficients and a time.
+
+    Args
+        c: List of coefficients generated by a quintic polynomial 
+            trajectory generator.
+        t: Time at which to calculate the acceleration
+
+    Returns
+        Acceleration
+    """
+    return 20*c[0]*t**3 + 12*c[1]*t**2 + 6*c[2]*t + 2*c[3]
+
+def rotation_matrix(roll, pitch, yaw):
+    """
+    Calculates the ZYX rotation matrix.
+
+    Args
+        Roll: Angular position about the x-axis in radians.
+        Pitch: Angular position about the y-axis in radians.
+        Yaw: Angular position about the z-axis in radians.
+
+    Returns
+        3x3 rotation matrix as NumPy array
+    """
+    return np.array(
+        [[cos(yaw)*cos(pitch), -sin(yaw)*cos(roll)+cos(yaw)*sin(pitch)*sin(roll), sin(yaw)*sin(roll)+cos(yaw)*sin(pitch)*cos(roll)],
+         [sin(yaw)*cos(pitch), cos(yaw)*cos(roll)+sin(yaw)*sin(pitch)*sin(roll), -cos(yaw)*sin(roll)+sin(yaw)*sin(pitch)*cos(roll)],
+         [-sin(pitch), cos(pitch)*sin(roll), cos(pitch)*cos(yaw)]
+        ])
+
+def main():
+    """
+    Calculates the x, y, z coefficients for the four segments 
+    of the trajectory
+    """
+    x_coeffs = [[], [], [], []]
+    y_coeffs = [[], [], [], []]
+    z_coeffs = [[], [], [], []]
+    waypoints = [[-5, -5, 5], [5, -5, 5], [5, 5, 5], [-5, 5, 5]]
+
+    for i in range(4):
+        traj = TrajectoryGenerator(waypoints[i], waypoints[(i+1)%4], T)
+        traj.solve()
+        x_coeffs[i] = traj.x_c
+        y_coeffs[i] = traj.y_c
+        z_coeffs[i] = traj.z_c
+
+    quad_sim(x_coeffs, y_coeffs, z_coeffs)
+
+if __name__ == "__main__":
+    main()