Direct Adaptive Disturbance Rejection and Control for a Deployable Space Telescope, Theory and Application Conference Paper

abstract

• Discrete time direct adaptive control with disturbance rejection is derived using the command tracker generator (CGT) design. A proof of stability for this controller is provided and the special case of adaptive disturbance rejection using a fixed gain controller is considered Preliminary results of the simplified adaptive controller performance on the Deployable Optical Telescope (DOT) prove promising, but overall reduction of observed motion in the multi-input, multi-output system is not easily achieved.

name of conference

• Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148)

authors

• Balas, Mark

published proceedings

• Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148)

author list (cited authors)

• Fuentes, R. J., Schrader, K. N., Balas, M. J., & Erwin, R. S.

citation count

• 14

complete list of authors

• Fuentes, Robert J||Schrader, Karl N||Balas, Mark J||Erwin, R Scott

publication date

• January 2001

publisher

• Institute of Electrical and Electronics Engineers (IEEE)  Publisher

published in

• Proceedings of the ... American Control Conference. American Control Conference  Journal

keywords

• Adaptive Control
• Adaptive Disturbance Rejection
• Adaptive Optics
• Aerospace Instrumentation
• Command Tracker Generator
• Control Systems
• Controller
• Deployable Optical Telescope
• Direct Adaptive Control
• Discrete Time Systems
• Disturbance Rejection
• Fixed Gain Controller
• Mimo Systems
• Model Reference Adaptive Control Systems
• Motion Control
• Multi-input Multi-output System
• Optical Control
• Performance Gain
• Programmable Control
• STABILITY
• Space Telescope
• Telescopes
• Tracking
• Us Department Of Transportation

Digital Object Identifier (DOI)

• 10.1109/acc.2001.946294

start page

• 3980

end page

• 3985

volume

• 5

URL

• http://dx.doi.org/10.1109/acc.2001.946294