Robust PD+ Control Algorithm for Satellite Attitude Tracking for Dynamic Targets
Author:
Affiliation:
1. School of Automation, Northwestern Polytechnical University, Xi’an, China
2. School of Aerospace Science and Technology, Xidian University, Xi’an, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
Hindawi Limited
Subject
General Engineering,General Mathematics
Link
http://downloads.hindawi.com/journals/mpe/2021/6680994.pdf
Reference21 articles.
1. Quaternion feedback for spacecraft large angle maneuvers
2. Quarternion feedback regulator for spacecraft eigenaxis rotations
3. Passivity-based attitude control on the special orthogonal group of rigid body rotations;R. F. James;Journal of Guidance, Control and Dynamics,2013
4. Robust tracking control design for spacecraft under control input saturation;D. B. Jovan;Journal of Guidance, Control and Dynamics,2004
5. Rapid Rotational Maneuvering of Rigid Satellites with Hybrid Actuators Configuration
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2. Synthesis of Data-Driven LightGBM Controller for Spacecraft Attitude Control;IEEE Access;2023
3. Finite-Time Controller for Flexible Satellite Attitude Fast and Large-Angle Maneuver;Symmetry;2021-12-30
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