An approximate optimal control method for 6-DOF spacecraft

Author:

Mao Renhao,Sun Shujian,Lei Jiakun

Abstract

Abstract In this paper, an approximate optimal control method based on adaptive dynamic programming (ADP) is proposed for the proximity operations with six degrees of freedom (6-DOF) relative motion control of spacecraft. Firstly, the dynamic model is normalized and dimension-reduced to avoid the excessive gradient change of the neural network. Then, a nonlinear disturbance observer is designed to deal with the disturbance. Finally, using ADP ‘s reinforcement learning idea, a single-critic neural network is constructed to solve the approximate optimal control strategy and minimize the cost function. The simulation results show that the designed controller can achieve the attitude and orbit maneuvering targets, and the overall energy consumption is approximately optimal.

Publisher

IOP Publishing

Reference10 articles.

1. Velocity-free finite-time relative 6-DOF control for rigid spacecraft;Ma;Advances in Space Research,2023

2. Backstepping-Based Six Degrees of Freedom Adaptive Control for Spacecraft Tracking a Noncooperative Target;Zhu;Journal of Circuits, Systems and Computers,2023

3. Fault-tolerant model-free predictive control of spacecraft coupled rotational–translational relative motion;Chiniforoushan;Journal of Aerospace Engineering,2021

4. Neural-network-based online HJB solution for optimal robust guaranteed cost control of continuous-time uncertain nonlinear systems;Liu;IEEE transactions on cybernetics,2014

5. ADP-based spacecraft attitude control under actuator misalignment and pointing constraints;Yang;IEEE Transactions on Industrial Electronics,2021

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