Comparative Synthesis of Linear and Nonlinear Attitude Controllers for LEO Satellite at Stabilization Mode
Author:
Affiliation:
1. Military Technical College M.T.C,Automatic Control Department,Cairo,Egypt
2. Military Technical College M.T.C,Aircraft Electrical Equipment Department,Cairo,Egypt
3. Military Technical College M.T.C,Guidance Department,Cairo,Egypt
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10206047/10206045/10206180.pdf?arnumber=10206180
Reference16 articles.
1. Dynamic sliding mode-based attitude stabilisation control of satellites with angular velocity and control constraints
2. Comparative Synthesis of Linear and Optimal Controllers for a Quadcopter Unmanned Aerial Vehicles
3. Twistor-based synchronous sliding mode control of spacecraft attitude and position;qing;Chinese Journal of Aeronautics,2018
4. Satellite attitude maneuver using sliding mode control under body angular velocity constraints;el-s;International Journal of Computer Applications,2012
5. Comparative Synthesis of Finite and Infinite Optimal Controllers for a Quadcopter with Input Constraints
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