Research Article

Model-Free Attitude Control of Spacecraft Based on PID-Guide TD3 Algorithm

Table 2

Hyperparameter settings.

HyperparametersSymbolValue

Random seedā€”2
Max episodes400
Max steps per episode200
Sample time1
Replay buffer size106
Batch size250
Policy network learning rate0.0003
Critic network learning rate0.001
Exploration noise scale0.1
Delay update3
Discount factor0.99
Soft update rate0.01