Efficient Event-Based Adaptive Sliding Mode Control for Spacecraft Attitude Stabilization
Author:
Affiliation:
1. Indian Institute of Technology Delhi, New Delhi 110 016, India
2. Indian Institute of Science Bangalore, Bangalore 560 012, India
3. King Abdulaziz University, Jeddah 21589, Saudi Arabia
4. Taif University, Taif 21944, Saudi Arabia
Funder
Deanship of Scientific Research (DSR), King Abdulaziz University, Jeddah
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G006080
Reference36 articles.
1. Plug-and-play satellites
2. Event-triggered communication and control of networked systems for multi-agent consensus
3. H-infinity Inverse Optimal Attitude-Tracking Control of Rigid Spacecraft
4. Attitude Tracking of Rigid Spacecraft With Bounded Disturbances
5. Attitude stabilization of rigid spacecraft with finite-time convergence
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