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dc.contributor.authorOland, Espen
dc.date.accessioned2019-04-08T11:02:18Z
dc.date.available2019-04-08T11:02:18Z
dc.date.issued2018-11-05
dc.description.abstractThe attitude determination and control system (ADCS) for spacecraft is responsible for determining its orientation using sensor measurements and then applying actuation forces to change the orientation. This chapter details the different components required for a complete attitude determination and control system for satellites moving in elliptical orbits. Specifically, the chapter details the orbital mechanics; perturbations; controller design; actuation methods such as thrusters, reaction wheels, and magnetic torquers; actuation modulation methods such as bang-bang, pulse-width modulation, and pulse-width pulse-frequency; as well as attitude determination using vector measurements combined with mathematical models. In sum, the work describes in a tutorial manner how to put everything together to enable the design of a complete satellite simulator.en_US
dc.descriptionSource at: <a href=https://www.intechopen.com/books/applied-modern-control/modeling-and-attitude-control-of-satellites-in-elliptical-orbits>https://www.intechopen.com/books/applied-modern-control/modeling-and-attitude-control-of-satellites-in-elliptical-orbits</a>en_US
dc.identifier.citationOland, E. (2018) Modeling and Attitude Control of Satellites in Elliptical Orbits. I Tuan, L.A.T. <i> Applied Modern Control </i> (s.151-178). London: IntechOpen. http://dx.doi.org/10.5772/intechopen.80422.en_US
dc.identifier.cristinIDFRIDAID 1665519
dc.identifier.doi10.5772/intechopen.80422
dc.identifier.isbn978-1-78984-827-4
dc.identifier.urihttps://hdl.handle.net/10037/15170
dc.language.isoengen_US
dc.publisherIntechOpenen_US
dc.relation.urihttps://www.intechopen.com/books/applied-modern-control/modeling-and-attitude-control-of-satellites-in-elliptical-orbits
dc.rights.accessRightsopenAccessen_US
dc.subjectVDP::Technology: 500::Electrotechnical disciplines: 540::Other electrotechnical disciplines: 549en_US
dc.subjectVDP::Teknologi: 500::Elektrotekniske fag: 540::Andre elektrotekniske fag: 549en_US
dc.titleModeling and Attitude Control of Satellites in Elliptical Orbitsen_US
dc.typePeer revieweden_US
dc.typeChapteren_US


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