BTT autopilot design using H∞ control theory

De Fu Lin; Bao Cai Sun; Jiang Wang

BTT autopilot design using H_∞ control theory

De Fu Lin^*
, Bao Cai Sun
, Jiang Wang

^*Corresponding author for this work

School of Aerospace Engineering

Academe of Air Force Equipment

Research output: Contribution to journal › Article › peer-review

4 Citations (Scopus)

Abstract

The H_∞ control problem was proposed in the BTT autopilot design, among which the selection of the weight function and the establishment of the mode were the main focus. Firstly the ideal mathematical model of BTT missile was established in pitch, yaw-roll coupled form. According to the design demand the weight functions were selected and the augmented model was built up. Then the pitch and lateral autopilot were designed using H_∞ theory.

Original language	English
Pages (from-to)	991-995
Number of pages	5
Journal	Xitong Fangzhen Xuebao / Journal of System Simulation
Volume	22
Issue number	4
Publication status	Published - Apr 2010

Keywords

Autopilot
BTT
BTT missile
H theory

Cite this

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title = "BTT autopilot design using H∞ control theory",

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AU - Sun, Bao Cai

AU - Wang, Jiang

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AB - The H∞ control problem was proposed in the BTT autopilot design, among which the selection of the weight function and the establishment of the mode were the main focus. Firstly the ideal mathematical model of BTT missile was established in pitch, yaw-roll coupled form. According to the design demand the weight functions were selected and the augmented model was built up. Then the pitch and lateral autopilot were designed using H∞ theory.

KW - Autopilot

KW - BTT

KW - BTT missile

KW - H theory

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BTT autopilot design using H_∞ control theory

Abstract

Keywords

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