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3D heading

Hold a target altitude and turn onto and hold a target heading with the 3D airliner, using throttle, elevator and aileron. The aileron commands a roll rate, not a bank angle, so heading is controlled through a cascade of two integrators, and the turbulence is hidden.

import target_gym as tg

env, params = tg.make("plane3d_heading")
Action space Box((3,)), all actions in [-1, 1]
Observation space Box((15,))
Tracked variable(s) altitude (m)
Episode length 300 steps of 1 s (5 min)
Cite as plane3d_heading-v4
Physics contract

Action space

Actions are normalised to [-1, 1] and mapped onto the plant's real actuator range inside the environment.

# meaning min max
0 power -1 1
1 stick -1 1
2 aileron -1 1

Observation space

15 values in the plant's own units. The space declares no bounds (it spans the float32 range), so scale them before training. The reward scores obs[2] against obs[10].

# meaning
0 x_dot, velocity along world x (m/s)
1 y_dot, velocity along world y (m/s)
2 z, altitude (m)
3 z_dot, vertical speed (m/s)
4 theta, pitch angle (rad)
5 theta_dot, pitch rate (rad/s)
6 phi, bank angle (rad)
7 phi_dot, roll rate (rad/s)
8 gamma, flight-path angle (rad)
9 psi, heading (rad)
10 target altitude (m)
11 target heading (rad)
12 throttle, 0 to 1
13 elevator deflection (rad)
14 aileron deflection (rad)

Rewards

See the environment's compute_reward.

Every environment in this suite scores on one contract. The reward is minus the sum of three non-negative costs, -(tracking_cost + running_cost + failure_cost). The running cost charges consumption and the failure cost charges trips out of the operating envelope. The reward is never positive, and its scale differs by orders of magnitude between plants. Some plants are priced in dollars or euros and the rest are dimensionless; the per-plant summary says which. See Reward shaping for how each cost is built.

Starting state

reset samples the initial condition and the target; state has 27 fields.

Episode end

Termination. None by default. Leaving the operating envelope trips the plant: the step that leaves it is charged the trip cost and sets info["tripped"] and info["trip_cost"], and the plant restarts as reset_env would while the episode clock keeps running. Episodic use is optional: with continuing = False the plant is lost and terminated is raised on that step instead. See Reward shaping.

Truncation. After 300 steps.

Baselines

Recorded over 10 seeds of the 300-step episode (see Baseline results). The reward is a cost, so a return closer to zero is better.

controller mean return cost per step
PID -1.672e+06 5573
MPC -6.893e+05 2298

The MPC beats the PID on 9 of 10 seeds and does not trip the plant on any of them.

Arguments

The scored configuration, which tg.make returns. A keyword argument changes one field, as in tg.make("plane3d_heading", max_steps_in_episode=...).

parameter value unit
delta_t 1 s
max_steps_in_episode 300 steps
gravity 9.81 m/s^2
initial_mass 73500 kg
thrust_output_at_sea_level 240000 N
air_density_at_sea_level 1.225 kg/m^3
frontal_surface 12.6 m^2
wings_surface 122.6 m^2
C_x0 0.095 -
C_z0 0.9 -
initial_fuel_quantity 19088 kg
specific_fuel_consumption 0.0175 kg/(kN.s)
power_response_rate 0.05 1/s
stick_response_rate 0.9 1/s
aileron_response_rate 0.9 1/s
aspect_ratio 9.48 -
aileron_effectiveness 0.4 -
cl_alpha 0.08786 1/deg
cl0 0.2 -
cd0 0.02 -
k 0.045 -
aoa_stall 15 deg
CL_max 1.5 -
CL_min -1 -
aoa_stall_width 3 deg
M_crit 0.8 -
k_shock_stall 4 -
shock_stall_floor 0.25 -
k_drag 5 -
I 9000000 kg.m^2
I_x 2500000 kg.m^2
moment_arm_stabilizer 15 m
moment_arm_wings 1.5 m
stabilizer_surface 27 m^2
elevator_surface 10 m^2
wingspan 35.8 m
aileron_surface 6 m^2
moment_arm_aileron 14 m
C_lp -0.4 -
min_alt 0 m
max_alt 12191.4 m
precision_floor 1 m
heading_precision_floor 0.0087 rad
position_precision_floor 3 m
reward_version 2 -
e_floor_altitude 1 m
e_tol_altitude 0 m
e_floor_heading 0.0087 rad
e_floor_path 3 m
tracking_exponent 2 -
failure_cost 2.9729e+08 reward
restart_steps 3600 steps
rho_floor_tracking 0.344219 reward
rho_floor 0.344219 reward
figure8_altitude_amplitude 200 m
initial_z_dot 0 m/s
initial_x_dot 200 m/s
initial_y_dot 0 m/s
initial_theta_dot 0 deg/s
initial_theta 0 deg
initial_phi 0 deg
initial_phi_dot 0 deg/s
initial_heading 0 rad
initial_power 1 -
initial_stick 0 deg
initial_aileron 0 deg
wind_x 0 m/s
wind_y 0 m/s
wind_z 0 m/s
turbulence_sigma 1.2 m/s
turbulence_theta 0.2 1/s
wind_shear_x 0 1/s
wind_shear_y 0 1/s
shear_ref_alt 0 m