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

被引:7
|
作者
Menegatti, Danilo [1 ,2 ]
Giuseppi, Alessandro [1 ,2 ]
Pietrabissa, Antonio [1 ,2 ]
机构
[1] Univ Roma La Sapienza, Dept Comp Control & Management Engn Antonio Ruber, Via Ariosto 25, I-00185 Rome, Italy
[2] CRAT, Space Control Grp, Via Giovanni Nicotera 29, I-0019 Rome, Italy
关键词
Spacecraft Control; Model Predictive Control; Collision Avoidance; SATELLITE FORMATION; TRACKING CONTROL; ATTITUDE-CONTROL; CONSTELLATION; COORDINATION; ROTATION; DESIGN;
D O I
10.1109/MED54222.2022.9837252
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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.
引用
收藏
页码:564 / 570
页数:7
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