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