DocumentCode :
2983509
Title :
Aeroelastic interactions with flight control of transatmospheric vehicles
Author :
Swaim, R.L.
Author_Institution :
Oklahoma State Univ., Stillwater, OK, USA
fYear :
1988
fDate :
23-27 May 1988
Firstpage :
574
Abstract :
The research needed on structural dynamics interactions with digital body dynamics and stability augmentation systems to allow confidence in vehicle design are discussed. This includes high-temperature-gradient effects on two- and three-dimensional total-vehicle elastic mode shapes and natural frequencies; robust control laws tolerant of wide uncertainties in elastic mode data; and compatible mathematical models for dynamic analysis of structures exhibiting low-frequency shell-type elastic modes. The expected use of metal matrix and carbon-carbon composite materials and ceramics with internally circulated cooling fluid will greatly complicate proper modeling and analysis of these interactions
Keywords :
aerospace control; stability; ceramics; composite materials; digital body dynamics; elastic mode data; flight control; high-temperature-gradient effects; internally circulated cooling fluid; low-frequency shell-type elastic modes; natural frequencies; robust control laws; stability augmentation systems; structural dynamics interactions; total-vehicle elastic mode shapes; transatmospheric vehicles; vehicle design; Aerodynamics; Aerospace control; Frequency; Mathematical model; Robust control; Shape control; Stability; Uncertainty; Vehicle dynamics; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace and Electronics Conference, 1988. NAECON 1988., Proceedings of the IEEE 1988 National
Conference_Location :
Dayton, OH
Type :
conf
DOI :
10.1109/NAECON.1988.195064
Filename :
195064
Link To Document :
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