An analytical design method for the missile two-loop acceleration autopilot

Hui Wang; Defu Lin; Jiaxin Wang; Tao Song

doi:10.1007/978-3-642-34381-0_18

An analytical design method for the missile two-loop acceleration autopilot

Hui Wang^*, Defu Lin, Jiaxin Wang, Tao Song

^*Corresponding author for this work

School of Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

5 Citations (Scopus)

Abstract

According to the missile longitudinal dynamics expressed as the state space matrix form and the defined dynamics coefficient notations, the missile body transfer functions are deduced in detail. Using the thought of pole allocation, a detailed analytical methodology for designing the two-loop acceleration autopilot has been proposed. To get the exact gain crossover frequency of the autopilot, an unconstraint optimization problem is outlined. The design and simulation results show that the two-loop acceleration autopilot can stabilize the missiles with different static margins very well.

Original language	English
Title of host publication	System Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings
Pages	157-165
Number of pages	9
Edition	PART 1
DOIs	https://doi.org/10.1007/978-3-642-34381-0_18
Publication status	Published - 2012
Event	Asia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012 - Shanghai, China Duration: 27 Oct 2012 → 30 Oct 2012

Publication series

Name	Communications in Computer and Information Science
Number	PART 1
Volume	326 CCIS
ISSN (Print)	1865-0929

Conference

Conference	Asia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012
Country/Territory	China
City	Shanghai
Period	27/10/12 → 30/10/12

Keywords

analytical methodology
missile
static margin
two-loop autopilot

Access to Document

10.1007/978-3-642-34381-0_18

Cite this

Wang, H., Lin, D., Wang, J., & Song, T. (2012). An analytical design method for the missile two-loop acceleration autopilot. In System Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings (PART 1 ed., pp. 157-165). (Communications in Computer and Information Science; Vol. 326 CCIS, No. PART 1). https://doi.org/10.1007/978-3-642-34381-0_18

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title = "An analytical design method for the missile two-loop acceleration autopilot",

abstract = "According to the missile longitudinal dynamics expressed as the state space matrix form and the defined dynamics coefficient notations, the missile body transfer functions are deduced in detail. Using the thought of pole allocation, a detailed analytical methodology for designing the two-loop acceleration autopilot has been proposed. To get the exact gain crossover frequency of the autopilot, an unconstraint optimization problem is outlined. The design and simulation results show that the two-loop acceleration autopilot can stabilize the missiles with different static margins very well.",

keywords = "analytical methodology, missile, static margin, two-loop autopilot",

author = "Hui Wang and Defu Lin and Jiaxin Wang and Tao Song",

year = "2012",

doi = "10.1007/978-3-642-34381-0_18",

language = "English",

isbn = "9783642343803",

series = "Communications in Computer and Information Science",

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booktitle = "System Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings",

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note = "Asia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012 ; Conference date: 27-10-2012 Through 30-10-2012",

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Wang, H, Lin, D, Wang, J & Song, T 2012, An analytical design method for the missile two-loop acceleration autopilot. in System Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings. PART 1 edn, Communications in Computer and Information Science, no. PART 1, vol. 326 CCIS, pp. 157-165, Asia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012, Shanghai, China, 27/10/12. https://doi.org/10.1007/978-3-642-34381-0_18

An analytical design method for the missile two-loop acceleration autopilot. / Wang, Hui; Lin, Defu; Wang, Jiaxin et al.
System Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings. PART 1. ed. 2012. p. 157-165 (Communications in Computer and Information Science; Vol. 326 CCIS, No. PART 1).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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T1 - An analytical design method for the missile two-loop acceleration autopilot

AU - Wang, Hui

AU - Lin, Defu

AU - Wang, Jiaxin

AU - Song, Tao

PY - 2012

Y1 - 2012

N2 - According to the missile longitudinal dynamics expressed as the state space matrix form and the defined dynamics coefficient notations, the missile body transfer functions are deduced in detail. Using the thought of pole allocation, a detailed analytical methodology for designing the two-loop acceleration autopilot has been proposed. To get the exact gain crossover frequency of the autopilot, an unconstraint optimization problem is outlined. The design and simulation results show that the two-loop acceleration autopilot can stabilize the missiles with different static margins very well.

AB - According to the missile longitudinal dynamics expressed as the state space matrix form and the defined dynamics coefficient notations, the missile body transfer functions are deduced in detail. Using the thought of pole allocation, a detailed analytical methodology for designing the two-loop acceleration autopilot has been proposed. To get the exact gain crossover frequency of the autopilot, an unconstraint optimization problem is outlined. The design and simulation results show that the two-loop acceleration autopilot can stabilize the missiles with different static margins very well.

KW - analytical methodology

KW - missile

KW - static margin

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SN - 9783642343803

T3 - Communications in Computer and Information Science

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BT - System Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings

T2 - Asia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012

Y2 - 27 October 2012 through 30 October 2012

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An analytical design method for the missile two-loop acceleration autopilot

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