Authors:Â Raghwendra Kishore Singh, A.Chowdhury
Abstract:Â This article reports state feedback based stability augmentation system for airplane aviation .The aircraft motion in both longitudinal as well as lateral directions have been considered to improve the dynamic stability of the aircraft. The State feedback gain matrix has been derived using the Bass-Gura algorithm. Aircraft motion in longitudinal and in lateral direction have been studied with and without state feedback gain the designed algorithm is implemented on MATLAB/ SIMULINK software.
Keywords:Â Controllability, Observability, Transformation matrix
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