Distributed Control of 6-DOF Leader-Following Multi-Spacecraft Formation near an Asteroid Based on Scaled Twistors
Author:
Affiliation:
1. Unmanned System Research Institute, Northwestern Polytechnical University, Xi'an, China
2. Aerospace System Engineering Shanghai, Shanghai, China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Aerospace Engineering
Link
http://xplorestaging.ieee.org/ielx7/7/7778228/09851453.pdf?arnumber=9851453
Reference41 articles.
1. 6 DOF synchronized control for spacecraft formation flying with input constraint and parameter uncertainties
2. Finite-Time Dynamic Surface Antisaturation Control for Spacecraft Terminal Approach Considering Safety
3. Twistor-Based Adaptive Pose Control of Spacecraft for Landing on an Asteroid With Collision Avoidance
4. Observer and Command-Filter-Based Adaptive Fuzzy Output Feedback Control of Uncertain Nonlinear Systems
5. Neural network-based sliding mode control for atmospheric-actuated spacecraft formation using switching strategy
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1. Velocity-Free Attitude Control for Flexible Spacecraft With Global Finite-Time Convergence;IEEE Transactions on Circuits and Systems II: Express Briefs;2024-09
2. Distributed Control for Multiple Spacecraft System Near Asteroids with Event-Triggered Strategy;Journal of Guidance, Control, and Dynamics;2024-05
3. Dynamic event-triggered attitude synchronization of multi-spacecraft formation via a learning neural network control approach;Aerospace Science and Technology;2023-11
4. Homogeneous Finite-Time Pose Tracking of Leader–Following Spacecraft Formation Using a Twistor-Based Model;Electronics;2023-10-29
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