Nonlinear Adaptive Attitude Control of Spacecraft
- 1 May 1987
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Aerospace and Electronic Systems
- Vol. AES-23 (3) , 371-379
- https://doi.org/10.1109/taes.1987.310835
Abstract
A model reference adaptive control law is presented for largeangle rotational maneuvers of spacecraft using reaction jets. It isassumed that the various parameters of the spacecraft arecompletely unknown, and unknown but bounded disturbancetorques are acting on the spacecraft. The controller includes adynamic system in the feedback path. Simulation results arepresented to show that fast, large angle rotational maneuvers can beperformed using the adaptive controller in spite of uncertainty inthe system.Keywords
This publication has 8 references indexed in Scilit:
- Adaptive model following control of nonlinear robotic systemsIEEE Transactions on Automatic Control, 1985
- Exact nonlinear control of large angle rotational maneuversIEEE Transactions on Automatic Control, 1984
- Asymptotic Reproducibility in Nonlinear Systems and Attitude Control of GyrostatIEEE Transactions on Aerospace and Electronic Systems, 1984
- Adaptive control of systems containing uncertain functions and unknown functions with uncertain boundsJournal of Optimization Theory and Applications, 1983
- Nonlinear Optimal Feedback Regulation of Satellite Angular MonentaIEEE Transactions on Aerospace and Electronic Systems, 1982
- Optimal Continuous Torque Attitude ManeuversJournal of Guidance and Control, 1980
- Stability of nonautonomous systemsNonlinear Analysis, 1976
- Equilibrium attitude transitions of a three-rotor gyrostat in a circular orbit.AIAA Journal, 1973