Method of Missile Salvo Hardware-in-the-loop Simulation Based on Multi Scattering Center Analog Measurement

Authors

Baiting Liu, 1. Science and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, China; ;2. Beijing Complex Product Advanced Manufacturing Engineering Research Center, Beijing Simulation Center, Beijing 100854, China;
Xiaolei Wang, 1. Science and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, China; ;2. Beijing Complex Product Advanced Manufacturing Engineering Research Center, Beijing Simulation Center, Beijing 100854, China;
Chaolei Wang, 1. Science and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, China; ;2. Beijing Complex Product Advanced Manufacturing Engineering Research Center, Beijing Simulation Center, Beijing 100854, China;
Yuhui Tao, 1. Science and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, China; ;2. Beijing Complex Product Advanced Manufacturing Engineering Research Center, Beijing Simulation Center, Beijing 100854, China;
Zhaowei Yang, 1. Science and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, China; ;2. Beijing Complex Product Advanced Manufacturing Engineering Research Center, Beijing Simulation Center, Beijing 100854, China;

Abstract

Abstract: For the verification requirements of the hardware-in-the-loop simulation test of a missile salvo guidance control system, this paper proposes a hardware-in-the-loop simulation test method for anti-aircraft missile based on multi-scattering center simulation to study the simulation method of missile salvo and the control method of multi-scattering center simulation of complex radio frequency target. The hardware-in-the-loop simulation verification test was carried out by constructing a hardware-in-the-loop simulation verification system. The verification test results show that the method can simulate the first missile and the target. The seeker can stably track the multi-scatter target, the target analog signal output maintains high quality, and the seeker angle error is smoothly converged, which can effectively support the design and verification of guidance control algorithm for a certain type of missile.

Recommended Citation

Liu, Baiting; Wang, Xiaolei; Wang, Chaolei; Tao, Yuhui; and Yang, Zhaowei (2019) "Method of Missile Salvo Hardware-in-the-loop Simulation Based on Multi Scattering Center Analog Measurement," Journal of System Simulation: Vol. 30: Iss. 12, Article 30.
DOI: 10.16182/j.issn1004731x.joss.201812030
Available at: https://dc-china-simulation.researchcommons.org/journal/vol30/iss12/30

First Page

4732

Revised Date

2018-08-01

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.201812030

Last Page

4737

CLC

TJ43+9.2

Recommended Citation

Liu Baiting, Wang Xiaolei, Wang Chaolei, Tao Yuhui, Yang Zhaowei. Method of Missile Salvo Hardware-in-the-loop Simulation Based on Multi Scattering Center Analog Measurement[J]. Journal of System Simulation, 2018, 30(12): 4732-4737.

DOI

10.16182/j.issn1004731x.joss.201812030