Stability region analysis of the parasitic loop of the semi-strapdown homing seeker

Author:

Jianmei S1,Gaohua C1,Xianxiang C1,Lixia K2

Affiliation:

1. Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China

2. China Aerospace Science & Industry Corp, Beijing, China

Abstract

The stability of the parasitic loop induced by the disturbance rejection effect (DRE) of a semi-strapdown homing seeker (SSHS) is analysed in this paper. First, the seeker’s tracking controller is designed so as to have a simple structure and then the explicit relationships between the control parameters and the desired performance index is presented. Mathematical models of the DRE of the SSHS and the parasitic loop are then proposed. The approximate maximum magnitude of the seeker’s DRE as a function of the friction coefficient and the counter electromotive force coefficient is also given. Routh’s criterion is used to obtain the approximate stability region of the parasitic loop. The necessary and sufficient conditions which ensure the stability of the parasitic loop are directly related to the seeker’s control parameters. This approach provides direct theoretical support for the design of a seeker’s control system. Simulations are performed to verify the validity of the stability analysis performed on the parasitic loop.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Control and Systems Engineering

Reference11 articles.

1. Line-of-sight rate estimation and linearizing control of an imaging seeker in a tactical missile guided by proportional navigation

2. Direct versus indirect line of sight (LOS) stabilization

3. Zhou R. Study of stabilization technology and design of angle tracking system for missileborne strapdown antenna platform. Doctor’s Thesis, School of Electronics and Information Engineering, Beijing University of Aeronautics and Astronautics, 2004. (In Chinese).

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