A new pulse modulator for solid propellant attitude control motors

Qi Sun; Jun Zhou; Zhilei Ge

doi:10.4028/www.scientific.net/AMR.429.292

A new pulse modulator for solid propellant attitude control motors

Qi Sun, Jun Zhou, Zhilei Ge

School of Astronautics

Northwestern Polytechnical University Xian

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

Abstract

Antimissile interceptors with the attitude control motors (ACM) were researched. For solid propellant ACM, a pulse frequency modulation scheme is proposed, which is based on conventional PWPF modulator. The modulator extends the application of modulation control method to solid propellant ACM, and integrates it with a feedback of thrust estimation which is decided by location and thrust interaction factors. The stability of the new modulator was analyzed by Lyapunov method and a stability margin was given. Simulations show that the stability margin is conservative, but acceptable. Interceptor simulations using the modulator indicate that this technique provides closer-to-linear actuation than conventional bang-bang thruster control methods.

Original language	English
Title of host publication	Manufacturing Systems Engineering
Pages	292-297
Number of pages	6
DOIs	https://doi.org/10.4028/www.scientific.net/AMR.429.292
State	Published - 2012
Event	2011 International Symposium on Manufacturing Systems Engineering, ISMSE 2011 - Hong Kong, Hong Kong Duration: 17 Sep 2011 → 18 Sep 2011

Publication series

Name	Advanced Materials Research
Volume	429
ISSN (Print)	1022-6680

Conference

Conference	2011 International Symposium on Manufacturing Systems Engineering, ISMSE 2011
Country/Territory	Hong Kong
City	Hong Kong
Period	17/09/11 → 18/09/11

Keywords

Anti-missile interceptor
Attitude control motors
Direct lateral force
Pulse modulation
PWPF

Access to Document

10.4028/www.scientific.net/AMR.429.292

Cite this

@inproceedings{d0506cf4865343c6acfd09577ee98c4e,

title = "A new pulse modulator for solid propellant attitude control motors",

abstract = "Antimissile interceptors with the attitude control motors (ACM) were researched. For solid propellant ACM, a pulse frequency modulation scheme is proposed, which is based on conventional PWPF modulator. The modulator extends the application of modulation control method to solid propellant ACM, and integrates it with a feedback of thrust estimation which is decided by location and thrust interaction factors. The stability of the new modulator was analyzed by Lyapunov method and a stability margin was given. Simulations show that the stability margin is conservative, but acceptable. Interceptor simulations using the modulator indicate that this technique provides closer-to-linear actuation than conventional bang-bang thruster control methods.",

keywords = "Anti-missile interceptor, Attitude control motors, Direct lateral force, Pulse modulation, PWPF",

author = "Qi Sun and Jun Zhou and Zhilei Ge",

year = "2012",

doi = "10.4028/www.scientific.net/AMR.429.292",

language = "英语",

isbn = "9783037852774",

series = "Advanced Materials Research",

pages = "292--297",

booktitle = "Manufacturing Systems Engineering",

note = "2011 International Symposium on Manufacturing Systems Engineering, ISMSE 2011 ; Conference date: 17-09-2011 Through 18-09-2011",

}

TY - GEN

T1 - A new pulse modulator for solid propellant attitude control motors

AU - Sun, Qi

AU - Zhou, Jun

AU - Ge, Zhilei

PY - 2012

Y1 - 2012

N2 - Antimissile interceptors with the attitude control motors (ACM) were researched. For solid propellant ACM, a pulse frequency modulation scheme is proposed, which is based on conventional PWPF modulator. The modulator extends the application of modulation control method to solid propellant ACM, and integrates it with a feedback of thrust estimation which is decided by location and thrust interaction factors. The stability of the new modulator was analyzed by Lyapunov method and a stability margin was given. Simulations show that the stability margin is conservative, but acceptable. Interceptor simulations using the modulator indicate that this technique provides closer-to-linear actuation than conventional bang-bang thruster control methods.

AB - Antimissile interceptors with the attitude control motors (ACM) were researched. For solid propellant ACM, a pulse frequency modulation scheme is proposed, which is based on conventional PWPF modulator. The modulator extends the application of modulation control method to solid propellant ACM, and integrates it with a feedback of thrust estimation which is decided by location and thrust interaction factors. The stability of the new modulator was analyzed by Lyapunov method and a stability margin was given. Simulations show that the stability margin is conservative, but acceptable. Interceptor simulations using the modulator indicate that this technique provides closer-to-linear actuation than conventional bang-bang thruster control methods.

KW - Anti-missile interceptor

KW - Attitude control motors

KW - Direct lateral force

KW - Pulse modulation

KW - PWPF

UR - http://www.scopus.com/inward/record.url?scp=84862925443&partnerID=8YFLogxK

U2 - 10.4028/www.scientific.net/AMR.429.292

DO - 10.4028/www.scientific.net/AMR.429.292

M3 - 会议稿件

AN - SCOPUS:84862925443

SN - 9783037852774

T3 - Advanced Materials Research

SP - 292

EP - 297

BT - Manufacturing Systems Engineering

T2 - 2011 International Symposium on Manufacturing Systems Engineering, ISMSE 2011

Y2 - 17 September 2011 through 18 September 2011

ER -

A new pulse modulator for solid propellant attitude control motors

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Cite this