Dynamic Inversion Controller Design for Balloon-Launched Supersonic Aircraft

While balloon launch is one of the most cost-efficient ways to realize a supersonic flight experiment, it presents some issues for the controller. D-SEND#2 is one flight experiment of this kind which was carried out in 2015. An unpowered test vehicle was lifted to an altitude of 30 km by a balloon a...

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Veröffentlicht in:	TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2018, Vol.61(6), pp.248-257
Hauptverfasser:	NINOMIYA, Tetsujiro, SUZUKI, Hirokazu, KAWAGUCHI, Jun’ichiro
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft design Control systems design Control theory Controllers D-SEND Dynamic Inversion Economic conditions Experiments Flight conditions Flight control Flight tests GNC systems Guidance (motion) Guidance and Control Separation Sonic booms Supersonic aircraft Supersonic flight Test vehicles Timescale Separation
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