국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	DERIVATION AND DEFINITION OF A LINEAR AIRCRAFT MODEL
저자	Eugene L. Duke, Robert F. Antoniewicz and Keith D. Krambeer
Keyword	Aircraft models; Dynamic models; Equations of state; Flight mechanics; Linear systems.
URL	http://www.dfrc.nasa.gov/DTRS/1988/PDF/H-1391.pdf
보고서번호	NASA-RP-1207
발행년도	1988
출처	NASA Dryden Flight Research Center
ABSTRACT	A linear aircraft model for a rigid aircraft of constant mass flying over a flat, nonrotating earth is derived and defined. The derivation makes no assumptions of reference trajectory or vehicle symmetry. The linear system equations are derived and evaluated along a general trajectory and include both aircraft dynamics and observation variables.