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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 3: 73 - 75

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.03.041

MISSILES AND GUIDANCE TECHNOLOGY

A Simplified Approach for Designing a Stable Loop for Missile with Relaxed Static Stability

  • GUO Zhengyu ,
  • LIANG Xiaogeng ,
  • ZHANG Yatao
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2011-08-12

  Online published: 2025-05-29

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Abstract

Relaxed static stability is a new concept in missile design, and it is a new way to raise the flying speed, distance and maneuverability for missile. The definition of RSS missile and its advantage were described. A simplified method for designing a stable loop for the RSS missile autopilot was developed. The simulation results of feature points on its trajectory shows that this approach offers satisfactory control system performance, so it suits for RSS missile autopilot design.

Key words： air-to-air missile; relaxed static stability; autopilot

Cite this article

GUO Zhengyu , LIANG Xiaogeng , ZHANG Yatao . A Simplified Approach for Designing a Stable Loop for Missile with Relaxed Static Stability[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(3) : 73 -75 . DOI: 10.15892/j.cnki.djzdxb.2012.03.041

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