Derivation and Definition of a Linear Aircraft Model

By National Aeronautics and Space Administration

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. Duke, Eugene L. and Antoniewicz, Robert F. and Krambeer, Keith D. Armstrong Flight Research Center AIRCRAFT MODELS; DYNAMIC MODELS; EQUATIONS OF STATE; FLIGHT MECHANICS; LINEAR SYSTEMS; MATHEMATICAL MODELS; AERODYNAMIC FORCES; EQUATIONS OF MOTION; LINEARIZATION; NONLINEAR EQUATIONS; STABILITY DERIVATIVES...

• Format: Paperback
• Language: English
• ISBN: 1730989748
• ISBN13: 9781730989742
• Release Date: January 1
• Publisher: Independently Published
• Length: 110 Pages
• Weight: 0.60 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"