DocumentCode :
485950
Title :
Symmetric Linear Systems
Author :
Lewis, John ; Martin, Clyde
Author_Institution :
Ames Research Center, NASA, Moffett Field, CA 94035
fYear :
1983
fDate :
22-24 June 1983
Firstpage :
1182
Lastpage :
1183
Abstract :
A major limitation to the use of helicopters in heavy construction has been that the masses that can be effectively and safely transported are restricted. One solution was the construction of the so-called heavy-lift helicopters. However it has been established that there are physical and economic limitations to the payload that can be transported. It has been proposed to circumvent this limitation by using multiple helicopters to move a single mass. The concept has been flight tested for two helicopters (twinlift) and the results were encouraging but showed that automatic control would be necessary to make the concept successful. In this paper the authors present some initial models and explore some of the control-theoretic problems inherent in the twinlift problem. A simplified linear model is examined, and it is shown that certain natural control schemes are not feasible, but that it is possible to control the linear model while preserving the essential characteristics of twinlift profile.
Keywords :
Aerodynamics; Automatic control; Automatic testing; Damping; Helicopters; Linear systems; Mathematics; Military aircraft; NASA; Payloads;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1983
Conference_Location :
San Francisco, CA, USA
Type :
conf
Filename :
4788294
Link To Document :
بازگشت