Trim equations of motion for aircraft design: Turning flight, pull-up and push-over

AIAA Atmospheric Flight Mechanics Conference and Exhibit

Volumn , Issue , 2003, Pages

  Chudoba, Bernd ^a   Cook, Michael V ^b  

^a University of Oklahoma   (United States)

^b CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

CONCEPTUAL DESIGN PHASE; CONCEPTUAL DESIGN STAGES; DESIGN DECISION-MAKING; DEVELOPMENT POTENTIAL; SIX-DEGREE-OF-FREEDOM; STABILITY AND CONTROL; STEADY STATE EQUATION; UNCONVENTIONAL AIRCRAFT;

AIRCRAFT CONTROL; CONCEPTUAL DESIGN; DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION; FLIGHT CONTROL SYSTEMS; VEHICLES;

AIRCRAFT;

EID: 84896812823     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Chudoba, B., "Stability and Control of Conventional and Unconventional Aircraft Configurations - A Generic Approach," First Edition, Books on Demand GmbH, January 2002, ISBN3-8311-2982-7, www.amazon.de, www.amazon.co.uk
2. Chudoba, B., "Development of a Generic Stability and Control Methodology for the Conceptual Design of Conventional and Unconventional Aircraft Configurations," Ph.D. Thesis, College of Aeronautics, Cranfield University, April 2001
3. Nelms, W.P., "Applications of Oblique-Wing Technology - An Overview," AIAA Paper 76-943, September 1976
4. Li, P., Seebass, R., and Sobieczky, H., "The Oblique Flying Wing as the New Large Aircraft," ICAS 96-4.3.2, September 1996
5. Thelander, J.A., "Aircraft Motion Analysis," Technical Documentary Report FDL-TDR-64-70, March 1965
6. Maine, R.E., "Aerodynamic Derivatives for an Oblique Wing Aircraft Estimated From Flight Data by Using a Maximum Likelihood Technique," NASA TP 1336, October 1978
7. Etkin, B. and Reid, L.D., "Dynamics of Flight - Stability and Control," Third Edition, John Wiley & Sons, Inc., 1996
8. Brüning, G., Hafer, X., and Sachs, G., "Flugleistungen," Third Edition, Springer, 1993