DocumentCode :
158050
Title :
Pulse Phase modulation for on-off thruster pair
Author :
Runle Du ; Jiaqi Liu ; Li Zhang ; Lu Gao
Author_Institution :
Nat. Key Lab. of Sci. & Technol. on Test Phys. & Numerical Math., Beijing, China
fYear :
2014
fDate :
1-8 March 2014
Firstpage :
1
Lastpage :
8
Abstract :
On-Off thrusters have limitation both at minimum on-time and minimum off-time, so the output is nonlinear pulses. Use on-off thrusters to provide linear or near linear control force is a fundamental and important research topic. Existing previous works do not overcome the limitation of on-time and off-time constraints, so the output is only an approximation of demanded force output. In this paper, Pulse Phase modulation (PP) is proposed to generate linear output through on-off thruster pair. PP modulation exploited the dynamic output curve of thrusters. By adjusting phase difference of thruster pair that installed in the opposite direction, thrust output can be linear proportional to demanded force output. PP modulation breaks the limitation caused by minimum on-time and off-time, and thus achieves high continuity of thrust output. For practical engineering implementation, two approximate methods are proposed as double frequency phase modulation and quadruple frequency phase modulation. Theoretical analysis and experimental results are provided to prove that PP modulation can yield much better precision in stabilizing space vehicles.
Keywords :
phase modulation; PP; adjusting phase difference; double frequency phase modulation; dynamic output curve; force output; near linear control force; nonlinear pulses; onoff thruster pair; opposite direction; pulse phase modulation; quadruple frequency phase modulation; space vehicles stability; Attitude control; Frequency control; Frequency modulation; Fuels; Phase modulation; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2014 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5582-4
Type :
conf
DOI :
10.1109/AERO.2014.6836195
Filename :
6836195
Link To Document :
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