28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-5.3.1
GUIDANCE AND CONTROL LAW FOR D-SEND#2
J. Kawaguchi, T. Ninomiya, H. Suzuki
Keywords: flight control, supersonic flight, uav, dynamic inversion
This paper describes the guidance and control law for D-SEND#2, where flight tests are planned in 2013. The guidance law is designed in such a way that a reference trajectory is generated for a varying flight range. The attitude control law is developed using the hierarchy-structured dynamic inversion technique.
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