Model Predictive Control for Collision-free Spacecraft Formation with Artificial Potential Functions

Danilo Menegatti, A. Giuseppi, A. Pietrabissa
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引用次数: 4

Abstract

A collision-free formation control strategy for flying in formation is presented. A linear control law is developed by means of Model Predictive Control (MPC) via the dual-mode paradigm [1]. Collision avoidance is dealt with by using Artificial Potential Functions (APFs) to keep a desired safe distance from the obstacles. The main innovation in the proposed approach is that each spacecraft independently performs the collision avoidance manoeuvres and, as a consequence, the APFs-based collision avoidance control is in charge also of the collision avoidance between two spacecraft. The optimality of the solution is discussed and numerical simulations show the effectiveness of the proposed method.
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基于人工势函数的无碰撞航天器编队模型预测控制
提出了一种编队飞行的无碰撞编队控制策略。通过双模模型预测控制(MPC),建立了一种线性控制律[1]。避碰是利用人工势函数(Artificial Potential Functions, apf)来保持与障碍物的安全距离。该方法的主要创新之处在于每个航天器独立执行避碰机动,因此,基于apfs的避碰控制也负责两个航天器之间的避碰。讨论了该方法的最优性,数值仿真结果表明了该方法的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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