Simulation of large scale, spacecraft power systems using sparse-matrix solution techniques

被引:3
|
作者
Ayres, M
Wait, DL [1 ]
Le, T
Wiederholt, M
机构
[1] Boeing Co, Canoga Park, CA 91304 USA
[2] Raytheon Syst Co, Houston, TX 77058 USA
关键词
simulation; spacecraft; international space station; large-scale systems; Newton-Raphson's method; equation solver; electrical power;
D O I
10.1016/S0965-9978(00)00017-X
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A program for simulating dynamic, coupled electrical power and thermal-hydraulic systems utilizes a single method to solve for both system electrical currents and fluid flow-rates. The simulation has been applied to large spacecraft, aircraft, and terrestrial power systems. The core of the program is a network solver that combines Newton's method with techniques for solving large, linear systems. The solution of nodal equations for both the electrical and fluid networks enables a common representation of the networks that easily translates into an object-oriented design. The speed and efficiency of the method enables large, real-time simulations with hardware-in-the-loop and software-in-the-loop as well as faster-than-real-time simulations. An example of the method is presented for the energy-coupled electrical power system (420 x 420 matrix) and thermal control system (200 x 200 matrix) on the International Space Station. (C) 2000 Elsevier Science Ltd. All rights reserved.
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页码:593 / 598
页数:6
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