An algorithm for computer-aided design calculation of aircraft stability and controllability parameters

An algorithm is proposed for computer-aided calculation of required values of aircraft controlling moments and aerodynamic moment coefficients for stable fulfillment of flight trajectories specified by design flight performance.

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Bibliographische Detailangaben
Veröffentlicht in:	Russian aeronautics 2010-09, Vol.53 (3), p.277-282
1. Verfasser:	Gainutdinov, V. G.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Aircraft stability Algorithms Automotive Engineering Computer aided design Controllability Engineering Flight Dynamics and Control of Flight Vehicles Mathematical analysis Trajectories
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	An algorithm is proposed for computer-aided calculation of required values of aircraft controlling moments and aerodynamic moment coefficients for stable fulfillment of flight trajectories specified by design flight performance.
ISSN:	1068-7998 1934-7901
DOI:	10.3103/S1068799810030062