Tripathi, Abha and Padhi, Radhakant (2008) Robustness Study of a Dynamic Inversion Control Law for a High Performance Aircraft. In: Proceedings of the International Conference on Aerospace Science and Technology, 26-28 June 2008, Bangalore, India.
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In the design of °ight control system modeling uncertainties in the form of param-eter variations is one of the major problems. It is even more critical for high performance aircrafts,since such aircrafts are purposefully designed unstable to enhance their performance (especially ma-neuverability). Hence the °ight control system needs to be quite e®ective in both assuring accurate tracking of pilot commands, while simultaneously assuring overall stability of the aircraft. In addi-tion, the control system must also be su±ciently robust to cater for possible parameter variations and inaccuracies . The primary aim of this paper is to carry out a robustness study of a dynamic inversion based nonlinear control design for a high performance aircraft, which has been developed recently .
|Item Type:||Conference Paper|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||29 Sep 2011 05:03|
|Last Modified:||29 Sep 2011 05:03|
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