Observer-Based Adaptive Neural Networks Optimal Control for Spacecraft
Proximity Maneuver with State Constraints
Abstract
This paper proposes an adaptive neural network (NN) optimal control
approach for autonomous relative motion control of non-cooperative
spacecraft in proximity. The proposed method aims to minimize fuel
consumption under various challenges including model uncertainty, state
constraints, external disturbances, and input saturation. To account for
uncertain parameters of non-cooperative target and external
disturbances, we start by designing a NN disturbance observer.
Subsequently, a novel optimal control index function is presented. An
adaptive NN based on the actor-critic (A-C) framework and backstepping
theory is then utilized to approximate the solution of
Hamilton-Jacobi–Bellman (HJB) equation and obtain an optimal control
law. The Lyapunov framework is leveraged to establish the stability of
the closed-loop control system. Finally, numerical simulations are
conducted to assess the feasibility and effectiveness of the proposed
control scheme in comparison with an existing approach.