DocumentCode
1617528
Title
On the simulation of the Space Shuttle main engine
Author
De Abreu-Garcia, J.A. ; Mohammad, A. ; Hartley, T.T.
Author_Institution
Dept. of Electr. Eng., Akron Univ., OH, USA
fYear
1990
Firstpage
188
Abstract
The Space Shuttle main engine simulation is analyzed to determine the means to obtain a faster running simulation. In particular, the valve dynamics module is simulated using three different techniques: Euler´s method, Adams-Bashforth two-step method, and the matrix stability region placement two-step method. It is shown that, by choosing the integration method appropriately, a speed-up factor of about five can be achieved. The valve dynamics module simulation results are then used to make recommendations about the simulation of the Space Shuttle main engine
Keywords
aerospace computing; aerospace engines; aerospace simulation; digital simulation; rockets; space vehicles; Adams-Bashforth two-step method; Euler´s method; Space Shuttle main engine simulation; integration method; matrix stability region placement two-step method; valve dynamics module; Analytical models; Computational modeling; Engines; Nonlinear dynamical systems; Real time systems; Reduced order systems; Rockets; Space shuttles; Stability; Valves;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics Society, 1990. IECON '90., 16th Annual Conference of IEEE
Conference_Location
Pacific Grove, CA
Print_ISBN
0-87942-600-4
Type
conf
DOI
10.1109/IECON.1990.149135
Filename
149135
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