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2010•Unpublished venueRequires access

Design and analysis of missile two-loop autopilot with PI compensator under multi-constraints

Hui Wang, Defu Lin, Jiang Wang, Zhenxuan Cheng

Open publisher page 2 citations

Abstract

In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.

About this research paper

What this paper is about

In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.

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OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Method / approach

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Available abstract

In order to eliminate the static error, PI compensator was introduced to the classic two-loop autopilot and the contribution of PI was analyzed while the equivalent time constant estimates of two-loop autopilot with PI was discussed. Four different objective functions were introduced to the design procedures. It is concluded that it is the large gain at low frequency of PI solved the problem of static error.

Key concepts: Autopilot, Control theory (sociology), Loop (graph theory), Missile, Pi, PID controller, Missile guidance, Constant (computer programming)

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