Longitudinal dynamics of a perching aircraft concept

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 5764, Issue , 2005, Pages 192-202

  Wickenheiser, Adam ^a   Garcia, Ephrahim ^a   Waszak, Martin ^b  

^a Cornell University   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Aircraft; Bio inspired; Lifting line; Modeling; Morphing; Perching; Simulation

Indexed keywords

BIO-INSPIRED; LIFTING LINE; PERCHING;

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; LANDING; LIFT; MATHEMATICAL MODELS; STABILITY;

AIRCRAFT;

EID: 25144481517     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.601512     Document Type: Conference Paper

References (8)

1. nd AIAA "Unmanned Unlimited" Systems, Technologies, and Operations, 15-18 September 2003, San Diego, CA.
2. Weissinger, J., "The Lift Distribution of Swept-back Wings", NACA Technical Memorandum No. 1120, 1947.
3. Chiocchia, G., Tordella, D., Prössdorf, S. "The Lifting Line Equation for a Curved Wing in Oscillatory Motion", Z. Angew. Math. Mech., 77 (1997) 4.
4. Wickenheiser, A., Garcia, E. "Modeling and Control of Morphing Air Vehicles", 15th International Conference on Adaptive Structures and Technologies, October 24-27, 2004, Bar Harbor, ME.
5. DeYoung, J., Harper, C. W., "Theoretical Symmetric Span Loading At Subsonic Speeds For Wings Having Arbitrary Plan Form", NACA Report No. 921, 1948.
6. Zipfel, Peter H., Modeling and Simulation of Aerospace Vehicle Dynamics, American Institute of Aeronautics and Astronautics, Inc., Reston, 2000.
7. Schmidt, Louis V., Introduction to Aircraft Flight Dynamics, American Institute of Aeronautics and Astronautics, Inc., Reston, 1998.
8. Hoak, D.E. et al., The USAF Stability and Control Datcom, Air Force Wright Aeronautical Laboratories, TR-83-3048, Oct. 1960 (Revised 1978).