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Author = Seyed Kamal Hosseini Sani
Number of Articles: 2
Nonlinear Dynamic Inversion Fault Tolerant Control for Spacecraft  Â
Volume 8, Issue 2 , July 2015, , Pages 11-17
Abstract
In this paper, a continuous globally stable tracking control algorithm is proposed for spacecraft in the presence of unknown actuator failure. The design method is based on nonlinear dynamic inversion and  in contrast to traditional fault-tolerant control methods, the proposed ... Read MoreIntelligent Satellite Orbit Prediction Based on Time Series Analysis
Volume 7, Issue 3 , October 2014, , Pages 43-49