DocumentCode
2835350
Title
Uncertainty disturbance modeling and effect on hypersonic test vehicle
Author
Wang, Xin ; Sun, Shijie
Author_Institution
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
fYear
2010
fDate
26-28 May 2010
Firstpage
930
Lastpage
933
Abstract
Disturbance error mathematic model of unmanned hypersonic test vehicle (UHTV) is analyzed in the paper. To meet the requirement of UHTV flight integration test, the separation disturbance model, the stochastic wind speed model, and uncertainty model of elastic effect are designed. The aerodynamic uncertainty parameters during engine on and off in level flight are given.
Keywords
aerospace control; aircraft; modelling; remotely operated vehicles; stochastic systems; uncertain systems; UHTV flight integration test; disturbance error mathematic model; elastic effect; stochastic wind speed model; uncertainty disturbance modeling; unmanned hypersonic test vehicle; Aerodynamics; Computational fluid dynamics; Control system synthesis; Educational institutions; Force measurement; Ignition; Testing; Uncertainty; Vehicles; Wind speed; attitude control; disturbance model; hypersonic; wind speed;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2010 Chinese
Conference_Location
Xuzhou
Print_ISBN
978-1-4244-5181-4
Electronic_ISBN
978-1-4244-5182-1
Type
conf
DOI
10.1109/CCDC.2010.5498090
Filename
5498090
Link To Document