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position_hold.py
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position_hold.py
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#!/usr/bin/env python3
'''
Team ID: 2222
Author List: Pratham Patil, Nandan N, Sriram Radhakrishnan, Samuel Thomas
Filename: position_hold.py
Theme: eYRC Sentinel Drone
Class: Edrone
This python file runs a ROS-node of name drone_control which holds the position of e-Drone on the given dummy.
This node publishes and subsribes the following topics:
PUBLICATIONS SUBSCRIPTIONS
/drone_command /whycon/poses
/alt_error /pid_tuning_altitude
/pitch_error /pid_tuning_pitch
/roll_error /pid_tuning_roll
Rather than using different variables, use list. eg : self.setpoint = [1,2,3], where index corresponds to x,y,z ...rather than defining self.x_setpoint = 1, self.y_setpoint = 2
CODE MODULARITY AND TECHNIQUES MENTIONED LIKE THIS WILL HELP YOU GAINING MORE MARKS WHILE CODE EVALUATION.
'''
# Importing the required libraries
from cmath import pi
from edrone_client.msg import *
from geometry_msgs.msg import PoseArray
from std_msgs.msg import Int16
from std_msgs.msg import Int64
from std_msgs.msg import Float64
from pid_tune.msg import PidTune
import rospy
import time
class Edrone():
"""docstring for Edrone"""
def __init__(self):
rospy.init_node('drone_control') # initializing ros node with name drone_control
# This corresponds to your current position of drone. This value must be updated each time in your whycon callback
# [x,y,z,yaw_value]
self.drone_position = [0.0, 0.0, 0.0, 0.0]
# [x_setpoint, y_setpoint, z_setpoint, yaw_value_setpoint]
self.setpoint = [2, 2, 20, 0.0] # whycon marker at the position of the dummy given in the scene. Make the whycon marker associated with position_to_hold dummy renderable and make changes accordingly
#Declaring a cmd of message type edrone_msgs and initializing values
self.cmd = edrone_msgs()
self.cmd.rcRoll = 1500
self.cmd.rcPitch = 1500
self.cmd.rcYaw = 1500
self.cmd.rcThrottle = 1500
self.cmd.rcAUX1 = 1500
self.cmd.rcAUX2 = 1500
self.cmd.rcAUX3 = 1500
self.cmd.rcAUX4 = 1500
#initial setting of Kp, Kd and ki for [roll, pitch, throttle]. eg: self.Kp[2] corresponds to Kp value in throttle axis
#after tuning and computing corresponding PID parameters, change the parameters
self.Kp = [0.0, 0.0, 0.0, 0.0]
self.Ki = [0.0, 0.0, 0.0, 0.0]
self.Kd = [0.0, 0.0, 0.0, 0.0]
#-----------------------Add other required variables for pid here ----------------------------------------------
#self.error = self.setpoint - self.drone_position
self.prev_error = [0] * 4
#self.integral = [0,0,0,0]
#self.derivative = [0,0,0,0]
self.max_values = [2000] * 4
self.min_values = [1000] * 4
self.error_sum = [0] * 4
self.isfrstflght = True
# Hint : Add variables for storing previous errors in each axis, like self.prev_error = [0,0,0] where corresponds to [pitch, roll, throttle] # Add variables for limiting the values like self.max_values = [2000,2000,2000] corresponding to [roll, pitch, throttle]
# self.min_values = [1000,1000,1000] corresponding to [pitch, roll, throttle]
# You can change the upper limit and lower limit accordingly.
#----------------------------------------------------------------------------------------------------------
# # This is the sample time in which you need to run pid. Choose any time which you seem fit. Remember the stimulation step time is 50 ms
self.sample_time = 0.030 # in seconds
# Publishing /drone_command, /alt_error, /pitch_error, /roll_error
self.command_pub = rospy.Publisher('/drone_command', edrone_msgs, queue_size=1)
#------------------------Add other ROS Publishers here-----------------------------------------------------
self.command_pub_ae = rospy.Publisher('/alt_error',Float64, queue_size=1)
self.command_pub_pe = rospy.Publisher('/pitch_error',Float64, queue_size=1)
self.command_pub_re = rospy.Publisher('/roll_error',Float64, queue_size=1)
self.command_pub_yawe = rospy.Publisher('/yaw_error',Float64, queue_size=1)
#-----------------------------------------------------------------------------------------------------------
# Subscribing to /whycon/poses, /pid_tuning_altitude, /pid_tuning_pitch, pid_tuning_roll
rospy.Subscriber('/whycon/poses', PoseArray, self.whycon_callback)
rospy.Subscriber('/pid_tuning_altitude',PidTune,self.altitude_set_pid)
#-------------------------Add other ROS Subscribers here----------------------------------------------------
rospy.Subscriber('/pid_tuning_pitch', PidTune, self.pitch_set_pid)
rospy.Subscriber('/pid_tuning_roll', PidTune, self.roll_set_pid)
rospy.Subscriber('/pid_tuning_yaw', PidTune, self.yaw_set_pid)
rospy.Subscriber('/drone_yaw', Int16, self.yaw_callback)
#------------------------------------------------------------------------------------------------------------
self.arm() # ARMING THE DRONE
# Disarming condition of the drone
def disarm(self):
self.cmd.rcAUX4 = 1100
self.command_pub.publish(self.cmd)
rospy.sleep(1)
# Arming condition of the drone : Best practise is to disarm and then arm the drone.
def arm(self):
self.disarm()
self.cmd.rcRoll = 1500
self.cmd.rcYaw = 1500
self.cmd.rcPitch = 1500
self.cmd.rcThrottle = 1000
self.cmd.rcAUX4 = 1500
self.command_pub.publish(self.cmd) # Publishing /drone_command
rospy.sleep(2)
# Whycon callback function
# The function gets executed each time when /whycon node publishes /whycon/poses
def whycon_callback(self,msg):
self.drone_position[0] = msg.poses[0].position.x
#--------------------Set the remaining co-ordinates of the drone from msg----------------------------------------------
p = msg.poses[0]
self.drone_position[1:3] = [p.position.y, p.position.z]
'''
self.drone_position[1] = msg.poses[1].position.y
self.drone_position[2] = msg.poses[2].position.z
'''
#---------------------------------------------------------------------------------------------------------------
# Callback function for /pid_tuning_altitude
# This function gets executed each time when /tune_pid publishes /pid_tuning_altitude
def altitude_set_pid(self,alt):
self.Kp[2] = alt.Kp * 1 # This is just for an example. You can change the ratio/fraction value accordingly
self.Ki[2] = alt.Ki * 1
self.Kd[2] = alt.Kd * 1
#----------------------------Define callback function like altitide_set_pid to tune pitch, roll--------------
def pitch_set_pid(self, pitch):
self.Kp[1] = pitch.Kp * 0.001 # This is just for an example. You can change the ratio/fraction value accordingly
self.Ki[1] = pitch.Ki * 0.008
self.Kd[1] = pitch.Kd * 0.5
def roll_set_pid(self,roll):
self.Kp[0] = roll.Kp * 0.001 # This is just for an example. You can change the ratio/fraction value accordingly
self.Ki[0] = roll.Ki * 0.008
self.Kd[0] = roll.Kd * 0.5
def yaw_set_pid(self, yaw):
self.Kp[3] = yaw.Kp * 0.001 # This is just for an example. You can change the ratio/fraction value accordingly
self.Ki[3] = yaw.Ki * 0.008
self.Kd[3] = yaw.Kd * 0.5
def yaw_callback(self, yaw):
self.drone_position[3] = yaw.data
def run(self):
while self.setpoint:
print(len(self.setpoint),self.setpoint[0], self.setpoint[1], self.setpoint[2], self.setpoint[3])
if len(self.setpoint) == 4:
print("TARGET LOCKED")
while not ((max(max(self.prev_error),-min(self.prev_error)) < 0.5 ) and not self.isfrstflght):
self.isfrstflght = False
self.pid()
self.setpoint.pop(0)
self.isfrstflght = True
self.disarm()
print("disarming")
#----------------------------------------------------------------------------------------------------------------------
def pid(self):
#-----------------------------Write the PID algorithm here--------------------------------------------------------------
# Steps:
# 1. Compute error in each axis. eg: error[0] = self.drone_position[0] - self.setpoint[0] ,where error[0] corresponds to error in x...
errors = [dp - setp for dp, setp in zip(self.drone_position, self.setpoint)]
self.command_pub_re.publish(errors[0])
self.command_pub_pe.publish(errors[1])
self.command_pub_ae.publish(errors[2])
self.command_pub_yawe.publish(errors[3])
# 2. Compute the error (for proportional), change in error (for derivative) and sum of errors (for integral) in each axis. Refer "Understanding PID.pdf" to understand PID equation.
der_err = [ce - pr_e for ce, pr_e in zip(errors, self.prev_error)]
new_error_sum = [ce + es for ce, es in zip(errors, self.error_sum)]
# 3. Calculate the pid output required for each axis. For eg: calcuate self.out_roll, self.out_pitch, etc.
out_vals = [sum(p*q for p, q in zip(a, b)) for a, b in zip(zip(errors, new_error_sum, der_err), zip(self.Kp, self.Ki, self.Kd))]
# 4. Reduce or add this computed output value on the avg value ie 1500. For eg: self.cmd.rcRoll = 1500 + self.out_roll. LOOK OUT FOR SIGN (+ or -). EXPERIMENT AND FIND THE CORRECT SIGN
out_vals = [1500 + val for val in out_vals]
# 6. Limit the output value and the final command value between the maximum(2000) and minimum(1000)range before publishing. For eg : if self.cmd.rcPitch > self.max_values[1]:
def clamp(n, minn, maxn): return max(min(maxn,n), minn)
out_vals = [clamp(val, self.min_values[i], self.max_values[i]) for i, val in enumerate(out_vals)]
self.cmd.rcPitch = int(out_vals[0])
self.cmd.rcRoll = int(out_vals[1])
self.cmd.rcThrottle = int(out_vals[2])
self.cmd.rcYaw = int(out_vals[3])
# 7. Update previous errors.eg: self.prev_error[1] = error[1] where index 1 corresponds to that of pitch (eg)
self.prev_error = errors
print(self.prev_error)
# 8. Add error_sum
self.error_sum = new_error_sum
# 5. Don't run the pid continously. Run the pid only at the a sample time. self.sampletime defined above is for this purpose. THIS IS VERY IMPORTANT.
time.sleep(e_drone.sample_time)
#publish command to drone
self.command_pub.publish(self.cmd)
#------------------------------------------------------------------------------------------------------------------------
if __name__ == '__main__':
e_drone = Edrone()
time.sleep(2)
r = rospy.Rate(30) #specify rate in Hz based upon your desired PID sampling time, i.e. if desired sample time is 33ms specify rate as 30Hz
while not rospy.is_shutdown():
#e_drone.pid()
e_drone.run()
r.sleep()
e_drone.disarm()