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
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;
Conference_Titel :
Industrial Electronics Society, 1990. IECON '90., 16th Annual Conference of IEEE
Conference_Location :
Pacific Grove, CA
Print_ISBN :
0-87942-600-4
DOI :
10.1109/IECON.1990.149135