Show simple item record

dc.contributor.advisorVadali, Srinivas R.
dc.creatorKim, Euisok
dc.date.accessioned2024-02-09T20:48:11Z
dc.date.available2024-02-09T20:48:11Z
dc.date.issued1993
dc.identifier.urihttps://hdl.handle.net/1969.1/DISSERTATIONS-1479204
dc.descriptionVitaen
dc.descriptionMajor subject: Aerospace Engineeringen
dc.description.abstractThe purpose of this research is to investigate the dynamics of a tethered satellite system in which the flexibility of the tether is considered and to design control laws for the deployment and retrieval of the tethered subsatellite using a method based on the Lyapunov stability theory. The dynamics of the system considered is modelled with as little simplifications and assumptions as possible to keep the problem tractable and at the same time physically realistic. Effects of geometric nonlinearity is taken into account. The hybrid governing equations are discretized by using the Galerkin's method. The flexible tether is also modelled as a series of beads which are connected in series by massless springs. Several tension and reel rate feedback control laws for deployment and retrieval are designed using Lyapunov's method when flexibility of the tether is neglected. It was found that the tension control laws designed for the simplified system can have a stabilizing effect on the vibrations of the tether. The performance of the full dynamic system with the designed control laws is investigated via simulations using both the Galerkin and bead model. At the same time, observations regarding the dynamics of the system and the validity of using the Galerkin's discretization procedure for a variable length tether are investigated. It is shown that the effects of geometric nonlinearity is significant during retrieval and that when geometric nonlinearity is included, an artificial instability is introduced into the Galerkin model causing sudden divergence of the system response during retrieval. This behavior is reproduced even for a simplified two dimensional example problem. It was found that the bead model produces a response that is physically realistic. Simulation studies using the bead model show that when reel rate control laws are used, vibrations grow to the point where the system becomes unstable. However, the tension control laws successfully retrieve the tethered subsatellite and were found to be effective in damping the elastic longitudinal vibrations in the early stages of retrieval. A nonrecursive order-N method for efficiently simulating the bead model is also introduced. The feasibility of implementing the order-N method for parallel computation is investigated using two parallel computer architectures. It was found that, due mostly to communication time, the use of the parallel computers do not offer any improvement in overall computation time.en
dc.format.extentix, 121 leavesen
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.subjectMajor aerospace engineeringen
dc.subject.classification1993 Dissertation K49
dc.subject.lcshTethered satellitesen
dc.subject.lcshSpace vehiclesen
dc.subject.lcshControl systemsen
dc.subject.lcshSpace vehiclesen
dc.subject.lcshDynamicsen
dc.titleDynamics and control of tethered satellite systemsen
dc.typeThesisen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameDoctor of Philosophyen
thesis.degree.namePh. Den
thesis.degree.levelDoctorialen
dc.contributor.committeeMemberHuang, Garng M.
dc.contributor.committeeMemberJunkins, John L.
dc.contributor.committeeMemberKurdila, Andrew J.
dc.type.genredissertationsen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen
dc.publisher.digitalTexas A&M University. Libraries
dc.identifier.oclc32494056


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record

This item and its contents are restricted. If this is your thesis or dissertation, you can make it open-access. This will allow all visitors to view the contents of the thesis.

Request Open Access