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dc.contributor.advisorLange, Benjamin O.
dc.contributor.authorLuders, Ernest Celestino
dc.date.accessioned2012-08-09T19:31:45Z
dc.date.available2012-08-09T19:31:45Z
dc.date.issued1966-08
dc.identifier.urihttp://hdl.handle.net/10945/9464
dc.description.abstractTwo feedback control schemes which maximize a terminal quantity while satisfying specified terminal conditions are discussed and compared. The schemes are "based on a linear perturbation from a nominal non-optimal path which does not, in general, satisfy the terminal conditions. The methods have been programmed in the ALGOL computer language for evaluation and the programs are included in the appendices.en_US
dc.description.urihttp://www.archive.org/details/comparisonofstee00lude
dc.language.isoen_US
dc.publisherStanford Universityen_US
dc.subject.lcshAeronauticsen_US
dc.titleA comparison of steepest-ascent and second variational techniques in solving a restricted class of trajectory optimization problems.en_US
dc.typeThesisen_US
dc.contributor.departmentAeronautics and Astronautics
etd.thesisdegree.nameEngr. in Aeronautics and Astronauticsen_US
etd.thesisdegree.levelProfessional Degreeen_US
etd.thesisdegree.disciplineAeronauticsen_US
etd.thesisdegree.disciplineAstronauticsen_US
etd.thesisdegree.grantorStanford Universityen_US


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