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Pulse modulation for attitude control with thrusters subject to switching restrictions

Kienitz, Karl Heinz and Bals, Johann (2005) Pulse modulation for attitude control with thrusters subject to switching restrictions. Aerospace Science and Technology, 9, pp. 635-640. ELSEVIER. DOI: 10.1016/j.ast.2005.06.006.

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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

Document Type:Article
Title:Pulse modulation for attitude control with thrusters subject to switching restrictions
Authors:
AuthorsInstitution or Email of Authors
Kienitz, Karl HeinzUNSPECIFIED
Bals, JohannUNSPECIFIED
Date:November 2005
Journal or Publication Title:Aerospace Science and Technology
Volume:9
DOI:10.1016/j.ast.2005.06.006
Page Range:pp. 635-640
Publisher:ELSEVIER
Status:Published
Keywords:Pulse modulation, Attitude control, Thrusters, Aerospace control, Switching restrictions
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems & Cabin
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics > System Dynamics and Control (former Control Design Engineering)
Deposited By: Astrid Jaschinski
Deposited On:02 Feb 2006
Last Modified:12 Dec 2013 20:08

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