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Derivation and definition of a linear aircraft model
NTRS Full-Text: Click to View  [PDF Size: 2.9 MB]
Author and Affiliation:
Duke, Eugene L.(NASA Hugh L. Dryden Flight Research Center, Edwards, CA, United States)
Antoniewicz, Robert F.(NASA Hugh L. Dryden Flight Research Center, Edwards, CA, United States)
Krambeer, Keith D.(NASA Hugh L. Dryden Flight Research Center, Edwards, CA, United States)
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.
Publication Date: Aug 01, 1988
Document ID:
19890005752
(Acquired Nov 06, 1995)
Accession Number: 89N15123
Subject Category: AIRCRAFT STABILITY AND CONTROL
Report/Patent Number: NASA-RP-1207, H-1391, NAS 1.61:1207
Document Type: Technical Report
Publisher Information: United States
Contract/Grant/Task Num: RTOP 505-66-11
Financial Sponsor: NASA; United States
Organization Source: NASA Dryden Flight Research Center; Edwards, CA, United States
Description: 106p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: AIRCRAFT MODELS; DYNAMIC MODELS; EQUATIONS OF STATE; FLIGHT MECHANICS; LINEAR SYSTEMS; MATHEMATICAL MODELS; AERODYNAMIC FORCES; EQUATIONS OF MOTION; LINEARIZATION; NONLINEAR EQUATIONS; STABILITY DERIVATIVES
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