class MyClient(MultirotorClient):
def __init__(self, **kwargs):
super(MyClient, self).__init__(**kwargs)
self.client = MultirotorClient()
self.client.confirmConnection()
self.client.enableApiControl(True)
self.client.armDisarm(True)
#self.client.reset() # 실행 시 뒤에 코드가 무시될 수 있어 필요할 때만 주석 해제
self.client.takeoffAsync().join()
self.roll = PIDDouble()
self.pitch = PIDDouble()
# Set PID Gain
self.set_pid_gain()
#Save Flight Data
self.flight_data = pd.DataFrame()
self.flight_data['altitude'] = 0
self.now = None
# Drone Value
self.angle = {'pitch': None, 'roll': None, 'yaw': None}
self.rate = {'pitch': None, 'roll': None, 'yaw': None}
self.altitude = None
self.longitude = None
self.latitude = None
self.DT = 0.001
self.ccr = {1: None, 2: None, 3: None, 4: None, 'duration': 1}
self.motor = {1: 0.60001, 2: 0.60001, 3: 0.6, 4: 0.6, 'duration': 1}
def __del__(self):
self.now = time.localtime()
self.now = time.strftime('%d%H%M%S', self.now)
# self.flight_data.to_csv(f'data/simulation_data_{self.now}')
def run(self):
while 1:
start = time.time()
# Read Sensor Data
# IMU
self.read_angle()
self.read_rate()
# Barometer
self.read_altitude()
# GPS
self.read_gps()
# Save Data
self.flight_data['altitude'] = self.altitude
# PID Control
self.Double_Roll_Pitch_PID_Calculation(self.pitch, 0,
self.angle['pitch'],
self.rate['pitch'], self.DT)
self.Double_Roll_Pitch_PID_Calculation(self.roll, 0,
self.angle['roll'],
self.rate['roll'], self.DT)
# PWM
self.ccr[
1] = 84000 + 600 * 84 - self.pitch.IN.pid_result + self.roll.IN.pid_result
self.ccr[
2] = 84000 + 600 * 84 + self.pitch.IN.pid_result + self.roll.IN.pid_result
self.ccr[
3] = 84000 + 600 * 84 + self.pitch.IN.pid_result - self.roll.IN.pid_result
self.ccr[
4] = 84000 + 600 * 84 - self.pitch.IN.pid_result - self.roll.IN.pid_result
for i in range(4):
if self.ccr[i + 1] < 84000: self.ccr[i + 1] = 84000
elif self.ccr[i + 1] > 168000: self.ccr[i + 1] = 168000
self.ccr[i + 1] = (self.ccr[i + 1] - 84000) / 84000
# Write Motors
self.client.moveByMotorPWMsAsync(self.ccr[4], self.ccr[2],\
self.ccr[1], self.ccr[3], self.ccr['duration'])
# print('roll : ',self.angle['roll'],' pitch : ', self.angle['pitch'], ' yaw : ', self.angle['yaw'])
self.DT = time.time() - start
if keyboard.read_key() == 'q':
break
del self.client
def read_angle(self):
self.angle['pitch'], self.angle['roll'], self.angle['yaw'] = \
airsim.to_eularian_angles(self.client.getImuData('Imu', 'Drone1').orientation)
self.angle['pitch'] *= -1
def read_rate(self):
self.rate['roll'] = self.client.getImuData(
'Imu', 'Drone1').angular_velocity.x_val
self.rate['pitch'] = self.client.getImuData(
'Imu', 'Drone1').angular_velocity.y_val
self.rate['yaw'] = self.client.getImuData(
'Imu', 'Drone1').angular_velocity.z_val
self.rate['pitch'] *= -1
def read_altitude(self):
self.altitude = self.client.getBarometerData(
barometer_name='Barometer', vehicle_name='Drone1').altitude
def read_gps(self):
self.longitude = self.client.getGpsData(
'Gps', 'Drone1').gnss.geo_point.longitude
self.latitude = self.client.getGpsData(
'Gps', 'Drone1').gnss.geo_point.latitude
def set_pid_gain(self):
self.pitch.IN.kp = 104
self.pitch.IN.ki = 0
self.pitch.IN.kd = 7
self.pitch.OUT.kp = 14
self.pitch.OUT.ki = 0
self.pitch.OUT.kd = 3
self.roll.IN.kp = 104
self.roll.IN.ki = 0
self.roll.IN.kd = 7
self.roll.OUT.kp = 14
self.roll.OUT.ki = 0
self.roll.OUT.kd = 3
def Double_Roll_Pitch_PID_Calculation(
self,
axis: PIDDouble,
set_point_angle: float,
angle: float, # BNO080 Rotation Angle
rate: float, # ICM-20602 Angular Rate
DT: float # loop time
):
# *********** Double PID Outer Begin (Roll and Pitch Angular Position Control) *************#
# P calculation
axis.OUT.reference = set_point_angle
axis.OUT.meas_value = angle
axis.OUT.error = axis.OUT.reference - axis.OUT.meas_value
axis.OUT.p_result = axis.OUT.error * axis.OUT.kp
# I calculation, DT need to be given in every loop
axis.OUT.error_sum = axis.OUT.error_sum + axis.OUT.error * DT # Define summation of outer loop
OUT_ERR_SUM_MAX = 2000
OUT_ERR_SUM_MIN = -OUT_ERR_SUM_MAX
if axis.OUT.error_sum > OUT_ERR_SUM_MAX:
axis.OUT.error_sum = OUT_ERR_SUM_MAX
elif axis.OUT.error_sum < OUT_ERR_SUM_MIN:
axis.OUT.error_sum = OUT_ERR_SUM_MIN
axis.OUT.i_result = axis.OUT.error_sum * axis.OUT.ki # Calculate I result of outer loop
# D calculation
OUTER_DERIV_FILT_ENABLE = True
axis.OUT.error_deriv = -rate # Define derivative of outer loop (rate = ICM-20602 Angular Rate)
if not OUTER_DERIV_FILT_ENABLE:
axis.OUT.d_result = axis.OUT.error_deriv * axis.OUT.kd # Calculate D result of outer loop
else:
axis.OUT.error_deriv_filt = axis.OUT.error_deriv_filt * 0.4 + axis.OUT.error_deriv * 0.6 # filter for derivative
axis.OUT.d_result = axis.OUT.error_deriv_filt * axis.OUT.kd # Calculate D result of inner loop
axis.OUT.pid_result = axis.OUT.p_result + axis.OUT.i_result + axis.OUT.d_result # Calculate PID result of outer loop
# ************ Double PID Inner Begin (Roll and Pitch Angular Rate Control) **************#
axis.IN.reference = axis.OUT.pid_result # Set point of inner PID control is the PID result of outer loop (for double PID control)
axis.IN.meas_value = rate # ICM-20602 angular rate
# P calculation
axis.IN.error = axis.IN.reference - axis.IN.meas_value # Define error of inner loop
axis.IN.p_result = axis.IN.error * axis.IN.kp # Calculate P result of inner loop
# I calculation
axis.IN.error_sum = axis.IN.error_sum + axis.IN.error * DT # Define summation of inner loop
IN_ERR_SUM_MAX = 500
IN_ERR_SUM_MIN = -IN_ERR_SUM_MAX
if axis.IN.error_sum > IN_ERR_SUM_MAX:
axis.IN.error_sum = IN_ERR_SUM_MAX
elif axis.IN.error_sum < IN_ERR_SUM_MIN:
axis.IN.error_sum = IN_ERR_SUM_MIN
axis.IN.i_result = axis.IN.error_sum * axis.IN.ki # Calculate I result of inner loop
# D calculation
axis.IN.error_deriv = -(axis.IN.meas_value - axis.IN.meas_value_prev
) / DT # Define derivative of inner loop
axis.IN.meas_value_prev = axis.IN.meas_value # Refresh value_prev to the latest value
INNER_DERIV_FILT_ENABLE = True
if not INNER_DERIV_FILT_ENABLE:
axis.IN.d_result = axis.IN.error_deriv * axis.IN.kd # Calculate D result of inner loop
else:
axis.IN.error_deriv_filt = axis.IN.error_deriv_filt * 0.5 + axis.IN.error_deriv * 0.5 # filter for derivative
axis.IN.d_result = axis.IN.error_deriv_filt * axis.IN.kd # Calculate D result of inner loop
axis.IN.pid_result = axis.IN.p_result + axis.IN.i_result + axis.IN.d_result # Calculate PID result of inner loop
def Single_Yaw_Heading_PID_Calculation(
axis: PIDSingle,
set_point_angle: float,
angle: float, # BNO080 Rotation Angle
rate: float, # ICM-20602 Angular Rate
DT: float # loop time
):
# *********** Single PID Begin (Yaw Angular Position) *************#
axis.reference = set_point_angle # Set point of yaw heading @ yaw stick is center.
axis.meas_value = angle # Current BNO080_Yaw angle @ yaw stick is center.
# P Calculation
axis.error = axis.reference - axis.meas_value # Define error of yaw angle control
if (axis.error > 180):
axis.error -= 360
elif (axis.error < -180):
axis.error += 360
axis.p_result = axis.error * axis.kp # Calculate P result of yaw angle control
# I Calculation
axis.error_sum = axis.error_sum + axis.error * DT # Define summation of yaw angle control
axis.i_result = axis.error_sum * axis.ki # Calculate I result of yaw angle control
# D Calculation
axis.error_deriv = -rate # Define differentiation of yaw angle control
axis.d_result = axis.error_deriv * axis.kd # Calculate D result of yaw angle control
axis.pid_result = axis.p_result + axis.i_result + axis.d_result # Calculate PID result of yaw angle contro
def Single_Yaw_Rate_PID_Calculation(
axis: PIDSingle,
set_point_rate: float,
rate: float, # ICM-20602 Angular Rate
DT: float):
# *********** Single PID Begin (Yaw Angular Rate Control) *************#
axis.reference = set_point_rate # Set point of yaw heading @ yaw stick is not center.
axis.meas_value = rate # Current ICM20602.gyro_z @ yaw stick is not center.
# P calculation
axis.error = axis.reference - axis.meas_value # Define error of yaw rate control
axis.p_result = axis.error * axis.kp # Calculate P result of yaw rate control
# I calculation
axis.error_sum = axis.error_sum + axis.error * DT # Define summation of yaw rate control
axis.i_result = axis.error_sum * axis.ki # Calculate I result of yaw rate control
# D calculation
axis.error_deriv = -(
axis.meas_value - axis.meas_value_prev
) / DT # Define differentiation of yaw rate control
axis.meas_value_prev = axis.meas_value # Refresh value_prev to the latest value
axis.d_result = axis.error_deriv * axis.kd # Calculate D result of yaw rate control
axis.pid_result = axis.p_result + axis.i_result + axis.d_result # Calculate PID result of yaw control
# *******************************************************************#
def Double_Altitude_PID_Calculation(axis: PIDDouble,
set_point_altitude: float,
current_altitude: float, DT: float):
# *********** Double PID Outer Begin (Roll and Pitch Angular Position Control) *************#
axis.OUT.reference = set_point_altitude # Set point of outer PID control
axis.OUT.meas_value = current_altitude # Actual Altitude from Fusion
# P Calculation
axis.OUT.error = axis.OUT.reference - axis.OUT.meas_value # Define error of outer loop
axis.OUT.p_result = axis.OUT.error * axis.OUT.kp # Calculate P result of outer loop
# I Calculation
axis.OUT.error_sum = axis.OUT.error_sum + axis.OUT.error * DT # Define summation of outer loop
OUT_ERR_SUM_MAX = 500
OUT_ERR_SUM_MIN = -OUT_ERR_SUM_MAX
if axis.OUT.error_sum > OUT_ERR_SUM_MAX:
axis.OUT.error_sum = OUT_ERR_SUM_MAX
elif axis.OUT.error_sum < OUT_ERR_SUM_MIN:
axis.OUT.error_sum = OUT_ERR_SUM_MIN
axis.OUT.i_result = axis.OUT.error_sum * axis.OUT.ki # Calculate I result of outer loop
# D Calculation
axis.OUT.error_deriv = -(axis.OUT.meas_value -
axis.OUT.meas_value_prev) / DT
axis.OUT.meas_value_prev = axis.OUT.meas_value
OUTER_DERIV_FILT_ENABLE = True
if not OUTER_DERIV_FILT_ENABLE:
axis.OUT.d_result = axis.OUT.error_deriv * axis.OUT.kd # Calculate D result of outer loop
else:
axis.OUT.error_deriv_filt = axis.OUT.error_deriv_filt * 0.4 + axis.OUT.error_deriv * 0.6 # filter for derivative
axis.OUT.d_result = axis.OUT.error_deriv_filt * axis.OUT.kd # Calculate D result of inner loop
axis.OUT.pid_result = axis.OUT.p_result + axis.OUT.i_result + axis.OUT.d_result # Calculate PID result of outer loop
# ************ Double PID Inner Begin (Roll and Pitch Angular Rate Control) **************#
axis.IN.reference = axis.OUT.pid_result # Set point of inner PID control is the PID result of outer loop (for double PID control)
axis.IN.meas_value = -axis.OUT.error_deriv_filt # ICM-20602 angular rate
# P calculation
axis.IN.error = axis.IN.reference - axis.IN.meas_value # Define error of inner loop
axis.IN.p_result = axis.IN.error * axis.IN.kp # Calculate P result of inner loop
# I calculation
axis.IN.error_sum = axis.IN.error_sum + axis.IN.error * DT # Define summation of inner loop
IN_ERR_SUM_MAX = 500
IN_ERR_SUM_MIN = -IN_ERR_SUM_MAX
if axis.IN.error_sum > IN_ERR_SUM_MAX:
axis.IN.error_sum = IN_ERR_SUM_MAX
elif axis.IN.error_sum < IN_ERR_SUM_MIN:
axis.IN.error_sum = IN_ERR_SUM_MIN
axis.IN.i_result = axis.IN.error_sum * axis.IN.ki # Calculate I result of inner loop
# D calculation
axis.IN.error_deriv = -(axis.IN.meas_value - axis.IN.meas_value_prev
) / DT # Define derivative of inner loop
axis.IN.meas_value_prev = axis.IN.meas_value # Refresh value_prev to the latest value
INNER_DERIV_FILT_ENABLE = True
if not INNER_DERIV_FILT_ENABLE:
axis.IN.d_result = axis.IN.error_deriv * axis.IN.kd # Calculate D result of inner loop
else:
axis.IN.error_deriv_filt = axis.IN.error_deriv_filt * 0.5 + axis.IN.error_deriv * 0.5 # filter for derivative
axis.IN.d_result = axis.IN.error_deriv_filt * axis.IN.kd # Calculate D result of inner loop
axis.IN.pid_result = axis.IN.p_result + axis.IN.i_result + axis.IN.d_result # Calculate PID result of inner loop
if axis.IN.pid_result < -2100: axis.IN.pid_result = -2100
if axis.IN.pid_result > 16800: axis.IN.pid_result = 16800
def Double_GPS_PID_Calculation(axis: PIDDouble, set_point_gps: float,
gps: float, DT: float):
# *********** Double PID Outer Begin (Roll and Pitch Angular Position Control) *************#
axis.OUT.reference = set_point_gps # Set point of outer PID control
axis.OUT.meas_value = gps
# P calculation
axis.OUT.error = axis.OUT.reference - axis.OUT.meas_value # Define error of outer loop
axis.OUT.p_result = axis.OUT.error * axis.OUT.kp # Calculate P result of outer loop
# I calculation
axis.OUT.error_sum = axis.OUT.error_sum + axis.OUT.error * DT # Define summation of outer loop
OUT_ERR_SUM_MAX = 500
OUT_ERR_SUM_MIN = -OUT_ERR_SUM_MAX
if axis.OUT.error_sum > OUT_ERR_SUM_MAX:
axis.OUT.error_sum = OUT_ERR_SUM_MAX
elif axis.OUT.error_sum < OUT_ERR_SUM_MIN:
axis.OUT.error_sum = OUT_ERR_SUM_MIN
axis.OUT.i_result = axis.OUT.error_sum * axis.OUT.ki # Calculate I result of outer loop
# D calculation
axis.OUT.error_deriv = -(axis.OUT.meas_value - axis.OUT.meas_value_prev
) / DT # Define derivative of outer loop
axis.OUT.meas_value_prev = axis.OUT.meas_value
OUTER_DERIV_FILT_ENABLE = True
if not OUTER_DERIV_FILT_ENABLE:
axis.OUT.d_result = axis.OUT.error_deriv * axis.OUT.kd # Calculate D result of outer loop
else:
axis.OUT.error_deriv_filt = axis.OUT.error_deriv_filt * 0.4 + axis.OUT.error_deriv * 0.6 # filter for derivative
axis.OUT.d_result = axis.OUT.error_deriv_filt * axis.OUT.kd # Calculate D result of inner loop
axis.OUT.pid_result = axis.OUT.p_result + axis.OUT.i_result + axis.OUT.d_result # Calculate PID result of outer loop
# ************ Double PID Inner Begin (Roll and Pitch Angular Rate Control) **************#
axis.IN.reference = axis.OUT.pid_result # Set point of inner PID control is the PID result of outer loop (for double PID control)
axis.IN.meas_value = -axis.OUT.error_deriv
# P calculation
axis.IN.error = axis.IN.reference - axis.IN.meas_value # Define error of inner loop
axis.IN.p_result = axis.IN.error * axis.IN.kp # Calculate P result of inner loop
# I calculation
axis.IN.error_sum = axis.IN.error_sum + axis.IN.error * DT # Define summation of inner loop
IN_ERR_SUM_MAX = 500
IN_ERR_SUM_MIN = -IN_ERR_SUM_MAX
if axis.IN.error_sum > IN_ERR_SUM_MAX:
axis.IN.error_sum = IN_ERR_SUM_MAX
elif axis.IN.error_sum < IN_ERR_SUM_MIN:
axis.IN.error_sum = IN_ERR_SUM_MIN
axis.IN.i_result = axis.IN.error_sum * axis.IN.ki # Calculate I result of inner loop
# D calculation
axis.IN.error_deriv = -(axis.IN.meas_value - axis.IN.meas_value_prev
) / DT # Define derivative of inner loop
axis.IN.meas_value_prev = axis.IN.meas_value # Refresh value_prev to the latest value
INNER_DERIV_FILT_ENABLE = True
if not INNER_DERIV_FILT_ENABLE:
axis.IN.d_result = axis.IN.error_deriv * axis.IN.kd # Calculate D result of inner loop
else:
axis.IN.error_deriv_filt = axis.IN.error_deriv_filt * 0.5 + axis.IN.error_deriv * 0.5 # filter for derivative
axis.IN.d_result = axis.IN.error_deriv_filt * axis.IN.kd # Calculate D result of inner loop
axis.IN.pid_result = axis.IN.p_result + axis.IN.i_result + axis.IN.d_result # Calculate PID result of inner loop
class Drone(Thread):
def __init__(self, telemetry: Telemetry):
super(Drone, self).__init__()
self.daemon = True
self._exit = False
self.telemetry = telemetry
self.client: Optional[MultirotorClient] = None
self.connect()
self.controller = Controller(self.client, self.telemetry)
self.collision_type = CollisionType.NONE
def run(self):
while not self._exit:
try:
self._process()
except BufferError:
pass
except KeyboardInterrupt:
self.shutdown()
def _process(self):
self.update_telemetry()
if self.is_collision():
self.process_collision()
elif self.telemetry.collision_mode:
self.stop_collision()
else:
self.controller.check_progress()
time.sleep(0.1)
def shutdown(self):
self._exit = True
self.client.enableApiControl(False)
self.client.reset()
def connect(self):
self.client = MultirotorClient()
self.client.confirmConnection()
self.client.enableApiControl(True)
self.client.getBarometerData()
# region TELEMETRY
def update_telemetry(self):
multirotor_state = self.client.getMultirotorState()
self.telemetry.landed_state = multirotor_state.landed_state
self.telemetry.ned_position = multirotor_state.kinematics_estimated.position
self.telemetry.linear_velocity = multirotor_state.kinematics_estimated.linear_velocity
self.telemetry.gps_position = self.client.getGpsData().gnss.geo_point
self.telemetry.gps_home = self.client.getHomeGeoPoint()
self.telemetry.quaternion = self.client.simGetVehiclePose().orientation
self.get_front_camera_image()
self.get_bottom_camera_image()
def get_bottom_camera_image(self):
self.client.simSetCameraOrientation('0',
Quaternionr(0.0, -0.7, 0.0, 0.5))
bottom_camera_data = self.client.simGetImages([
airsim.ImageRequest("0",
airsim.ImageType.DepthPlanner,
pixels_as_float=True)
])
self.telemetry.terrain_collision.process_image(bottom_camera_data[0])
def get_front_camera_image(self):
self.client.simSetCameraOrientation('0',
Quaternionr(0.0, 0.0, 0.0, 1.0))
front_camera_data = self.client.simGetImages([
airsim.ImageRequest("0",
airsim.ImageType.DepthPlanner,
pixels_as_float=True)
])
self.telemetry.wall_collision.process_image(front_camera_data[0])
# endregion
# region COLLISION
def is_collision(self):
collision = (self.telemetry.wall_collision.collision
or self.telemetry.terrain_collision.collision)
return collision
def process_collision(self):
wall_collision = self.telemetry.wall_collision.collision
terrain_collision = self.telemetry.terrain_collision.collision
if wall_collision:
if terrain_collision:
self.wall_collision()
self.collision_type = CollisionType.BOTH
else:
self.wall_collision()
self.collision_type = CollisionType.WALL
else:
if terrain_collision:
self.terrain_collision()
self.collision_type = CollisionType.TERRAIN
else:
self.collision_type = CollisionType.NONE
def wall_collision(self):
if (self.collision_type != CollisionType.WALL
and self.collision_type != CollisionType.BOTH):
self.telemetry.collision_mode = True
self.client.moveToZAsync(-500, settings.COLLISION_SPEED)
def terrain_collision(self):
if self.collision_type != CollisionType.TERRAIN:
if self.telemetry.ned_position.z_val < -8:
self.telemetry.collision_mode = True
target = self.telemetry.target_position
actual = self.telemetry.ned_position
self.client.moveToPositionAsync(target.x_val, target.y_val,
actual.z_val - 1,
settings.COLLISION_SPEED)
def stop_collision(self):
self.controller.send_position()
self.telemetry.collision_mode = False
