Model Predictive Control-Based Guidance and Control System for Simultaneous Multi-Satellite Assembly in Proximity Operation
Author:
Affiliation:
1. United Arab Emirates University,Department of Mechanical and Aerospace Engineering,Al Ain,United Arab Emirates
Funder
United Arab Emirates University
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9852822/9852497/09852870.pdf?arnumber=9852870
Reference23 articles.
1. Motion planning and control for on-orbit assembly using lqr-rrt* and nonlinear mpc;doerr,2020
2. Artificial potential function based spacecraft proximity maneuver 6-dof control under multiple pyramid-type constraints;wang;ISA Transactions,2021
3. Autonomous Low-Thrust Control of Long-Distance Satellite Clusters Using Artificial Potential Function
4. Model Predictive Control for Spacecraft Rendezvous and Docking: Strategies for Handling Constraints and Case Studies
5. Model predictive control for spacecraft rendezvous in elliptical orbit
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Satellite Formation Keeping Based on Legendre Pseudospectral Method;2023 42nd Chinese Control Conference (CCC);2023-07-24
2. Autonomous assembly of multiple flexible spacecraft using RRT* algorithm and input shaping technique;Nonlinear Dynamics;2023-04-20
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