#!/usr/bin/env python ''' simple rover simulator core ''' from aircraft import Aircraft import util, time, math from math import degrees, radians from rotmat import Vector3, Matrix3 class Rover(Aircraft): '''a simple rover''' def __init__(self, max_speed=10, max_accel=10, max_turn_rate=45): Aircraft.__init__(self) self.max_speed = max_speed self.max_accel = max_accel self.max_turn_rate = max_turn_rate self.last_time = time.time() def update(self, state): # how much time has passed? t = time.time() delta_time = t - self.last_time self.last_time = t # speed in m/s in body frame velocity_body = self.dcm.transposed() * self.velocity # speed along x axis, +ve is forward speed = velocity_body.x # yaw rate in degrees/s yaw_rate = self.max_turn_rate * state.steering * (speed / self.max_speed) # target speed with current throttle target_speed = state.throttle * self.max_speed # linear acceleration in m/s/s - very crude model accel = self.max_accel * (target_speed - speed) / self.max_speed # print('speed=%f throttle=%f steering=%f yaw_rate=%f accel=%f' % (speed, state.throttle, state.steering, yaw_rate, accel)) self.gyro = Vector3(0,0,radians(yaw_rate)) # update attitude self.dcm.rotate(self.gyro * delta_time) self.dcm.normalize() # accel in body frame due to motor accel_body = Vector3(accel, 0, 0) # add in accel due to direction change accel_body.y += radians(yaw_rate) * speed # now in earth frame accel_earth = self.dcm * accel_body accel_earth += Vector3(0, 0, self.gravity) # if we're on the ground, then our vertical acceleration is limited # to zero. This effectively adds the force of the ground on the aircraft accel_earth.z = 0 # work out acceleration as seen by the accelerometers. It sees the kinematic # acceleration (ie. real movement), plus gravity self.accel_body = self.dcm.transposed() * (accel_earth + Vector3(0, 0, -self.gravity)) # new velocity vector self.velocity += accel_earth * delta_time # new position vector old_position = self.position.copy() self.position += self.velocity * delta_time # update lat/lon/altitude self.update_position(delta_time)