Abstract
Sections 1 through 4 of the full paper give the explanation of: ″the missions of and the requirements on the simulation system, the construction of the small-sized hardware-in-the-loop simulation system based on RT-LAB, and the procedure for simulation experiment.″ Section 5 gives the digital simulation results and the hardware-in-the-loop ones, and the contrast of these two types of simulation results. The results and their constrast, presented in Figs. 4, 5 and 6, and their analysis indicate preliminarily that: (1) the simulink model can be applied to the hardware-in-the-loop simulation system based on RT-LAB conveniently and rapidly; (2) the difficulty of establishing the system is reduced; (3) the development period is shortened; (4) the flexibility and reliability of the simulation system are enhanced.
| Original language | English |
|---|---|
| Pages (from-to) | 318-322 |
| Number of pages | 5 |
| Journal | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University |
| Volume | 28 |
| Issue number | 3 |
| State | Published - Jun 2010 |
Keywords
- Flight control systems
- Hardware-in-the-loop simulation
- Missiles
- RT-LAB
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