Research on the thrust vector control via jet vane in rapid turning of vertical launch

Fuxiang Liu; Liumin Wang

doi:10.1109/MIC.2013.6758092

Research on the thrust vector control via jet vane in rapid turning of vertical launch

Fuxiang Liu, Liumin Wang

School of Aerospace Engineering

Beijing Institute of Technology

Research output: Contribution to conference › Paper › peer-review

6 Citations (Scopus)

Abstract

In order to solve the problem of rapid turning of missile vertical launch, the thrust vector control of jet vane is designed in this paper. By applying the force analysis to the jet vane, the mathematical model of the missile's pitch motion in the vertical plane is established. At the same time the jet vane controller is designed, which introducing the missile's pitch angle position control and rate control. The simulation results show that the jet vane controller with the PID control rule can make the missile fast turn within one second. The model of jet vane thrust vector control can effectively provide sufficient control torque for a missile's quick turn.

Original language	English
Pages	837-842
Number of pages	6
DOIs	https://doi.org/10.1109/MIC.2013.6758092
Publication status	Published - 2013
Event	2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013 - Harbin, China Duration: 16 Aug 2013 → 18 Aug 2013

Conference

Conference	2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013
Country/Territory	China
City	Harbin
Period	16/08/13 → 18/08/13

Keywords

Digital simulation
Jet vane
Thrust vector control
Vertical launch

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10.1109/MIC.2013.6758092

Cite this

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title = "Research on the thrust vector control via jet vane in rapid turning of vertical launch",

abstract = "In order to solve the problem of rapid turning of missile vertical launch, the thrust vector control of jet vane is designed in this paper. By applying the force analysis to the jet vane, the mathematical model of the missile's pitch motion in the vertical plane is established. At the same time the jet vane controller is designed, which introducing the missile's pitch angle position control and rate control. The simulation results show that the jet vane controller with the PID control rule can make the missile fast turn within one second. The model of jet vane thrust vector control can effectively provide sufficient control torque for a missile's quick turn.",

keywords = "Digital simulation, Jet vane, Thrust vector control, Vertical launch",

author = "Fuxiang Liu and Liumin Wang",

year = "2013",

doi = "10.1109/MIC.2013.6758092",

language = "English",

pages = "837--842",

note = "2013 2nd International Conference on Measurement, Information and Control, ICMIC 2013 ; Conference date: 16-08-2013 Through 18-08-2013",

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AU - Liu, Fuxiang

AU - Wang, Liumin

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AB - In order to solve the problem of rapid turning of missile vertical launch, the thrust vector control of jet vane is designed in this paper. By applying the force analysis to the jet vane, the mathematical model of the missile's pitch motion in the vertical plane is established. At the same time the jet vane controller is designed, which introducing the missile's pitch angle position control and rate control. The simulation results show that the jet vane controller with the PID control rule can make the missile fast turn within one second. The model of jet vane thrust vector control can effectively provide sufficient control torque for a missile's quick turn.

KW - Digital simulation

KW - Jet vane

KW - Thrust vector control

KW - Vertical launch

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Y2 - 16 August 2013 through 18 August 2013

ER -

Research on the thrust vector control via jet vane in rapid turning of vertical launch

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