import math, util, rotmat from rotmat import Vector3, Matrix3 class Aircraft(object): '''a basic aircraft class''' def __init__(self): self.home_latitude = 0 self.home_longitude = 0 self.home_altitude = 0 self.ground_level = 0 self.frame_height = 0.0 self.latitude = self.home_latitude self.longitude = self.home_longitude self.altitude = self.home_altitude self.dcm = Matrix3() # rotation rate in body frame self.gyro = Vector3(0,0,0) # rad/s self.velocity = Vector3(0, 0, 0) # m/s, North, East, Down self.position = Vector3(0, 0, 0) # m North, East, Down self.mass = 0.0 self.update_frequency = 50 # in Hz self.gravity = 9.8 # m/s/s self.accelerometer = Vector3(0, 0, -self.gravity) self.wind = util.Wind('0,0,0') def on_ground(self, position=None): '''return true if we are on the ground''' if position is None: position = self.position return (-position.z) + self.home_altitude <= self.ground_level + self.frame_height def update_position(self, delta_time): '''update lat/lon/alt from position''' bearing = math.degrees(math.atan2(self.position.y, self.position.x)) distance = math.sqrt(self.position.x**2 + self.position.y**2) (self.latitude, self.longitude) = util.gps_newpos(self.home_latitude, self.home_longitude, bearing, distance) self.altitude = self.home_altitude - self.position.z velocity_body = self.dcm.transposed() * self.velocity # force the acceleration to mostly be from gravity. We should be using 100% accel_body, # but right now that flies very badly as the AHRS system can't do centripetal correction # for multicopters. This is a compromise until we get that sorted out accel_true = self.accel_body accel_fake = self.dcm.transposed() * Vector3(0, 0, -self.gravity) self.accelerometer = (accel_true * 0.5) + (accel_fake * 0.5)