Pulse modulation for attitude control with thrusters subject to switching restrictions

A pulse modulation scheme based on two modulation curves is proposed for applications in spacecraft attitude control using thrusters which may be subject to switching restrictions. These constraints are taken into account explicitly during the design of the modulation scheme which can implement arbi...

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Published inAerospace science and technology Vol. 9; no. 7; pp. 635 - 640
Main Authors Kienitz, Karl Heinz, Bals, Johann
Format Journal Article
LanguageEnglish
Published Paris Elsevier 01.10.2005
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Abstract A pulse modulation scheme based on two modulation curves is proposed for applications in spacecraft attitude control using thrusters which may be subject to switching restrictions. These constraints are taken into account explicitly during the design of the modulation scheme which can implement arbitrary bounded functions between constant modulator input and averaged modulator output.
AbstractList A pulse modulation scheme based on two modulation curves is proposed for applications in spacecraft attitude control using thrusters which may be subject to switching restrictions. These constraints are taken into account explicitly during the design of the modulation scheme which can implement arbitrary bounded functions between constant modulator input and averaged modulator output.
Author Bals, Johann
Kienitz, Karl Heinz
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Issue 7
Keywords Modulator
Attitude control
Aerospace
Spacecraft
Switching restrictions
Thrusters
Pulse modulation
Aerospace control
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SubjectTerms Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Physics
Solid dynamics (ballistics, collision, multibody system, stabilization...)
Solid mechanics
Title Pulse modulation for attitude control with thrusters subject to switching restrictions
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