$${H}_{\infty }$$ Approach to Performance Analysis of Missile Control Systems with Proportional Navigation Guidance Laws
| Autor: | Seong-Ho Song |
|---|---|
| Rok vydání: | 2021 |
| Předmět: |
010504 meteorology & atmospheric sciences
0211 other engineering and technologies Linear matrix inequality Order (ring theory) 02 engineering and technology 01 natural sciences Stability (probability) Missile autopilot Nonlinear system Missile Computer Science::Systems and Control Control system Law Proportional navigation Electrical and Electronic Engineering 021101 geological & geomatics engineering 0105 earth and related environmental sciences Mathematics |
| Zdroj: | Journal of Electrical Engineering & Technology. 16:1083-1088 |
| ISSN: | 2093-7423 1975-0102 |
| DOI: | 10.1007/s42835-020-00617-0 |
| Popis: | This paper presents a performance analysis of missile control systems considering nonlinear pursuit dynamics and proportional navigation guidance (PNG) laws. In order to analyze the system stability, missile dynamics are simplified as a linearized model which is often considered in missile autopilot design and the well-known $${{{H}}}_{\boldsymbol{\infty }}$$ approach is employed. A sufficient condition guaranteeing miss distance and the closed loop stability is proposed. The provided condition of missile system stability can be numerically easily verified by a linear matrix inequality (LMI). |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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