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dc.contributor.authorFahroo, Fariba
dc.contributor.authorRoss, I. Michael
dc.dateAugust 21-24, 2006
dc.date.accessioned2013-03-07T21:43:12Z
dc.date.available2013-03-07T21:43:12Z
dc.date.issued2006-08-21
dc.identifier.urihttps://hdl.handle.net/10945/29663
dc.descriptionThe article of record as published may be located at http://arc.aiaa.orgen_US
dc.descriptionProceedings of AIAA Guidance, Navigation, and Control Conference ; Paper no. AIAA 2006-6304, Keystone, Colorado, Aug. 21-24, 2006en_US
dc.description.abstractOne of the most efficient families of techniques for solving space trajectory optimization problems are pseudospectral (PS) methods. Among the rich variety of PS methods, the class of Legendre PS methods are most thoroughly studied for optimal control and trajectory optimization applications. In particular, the Legendre-Gauss-Lobatto PS method is widely used for boundary-value type problems while the Legendre-Gauss-Radau PS method was recently proposed for solving innate-horizon optimal control problems as a means to manage conditions at inanity. Both methods satisfy the Convector Mapping Principle, the mathematical principle associated with the consistency of approximations that allows one to generate dual maps (such as Hamiltonians, adjoins etc) without resorting to solving di'cult two-point boundary-value problems. In this paper we prove that a combination of weighted interpolants, their duals, and a proper definition of orthogonality allows us to formulate a generalized Covector Mapping Theorem that applies to all such PS methods. The consequences of this theorem are that it clarifies the connections between theory and computation, the impact of these connections on solving trajectory optimization problems, and the selection of the correct PS method for solving problems quickly and efficiently. A classical benchmark continuous-thrust orbit transfer problem is used to illustrate the concepts.en_US
dc.publisherThe American Institute of Aeronautics and Astronautics (AIAA)en_US
dc.relation.ispartofAIAA/AAS Astrodynamics Specialist Conference and Exhibit 21 - 24 August 2006, Keystone, Colorado
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleOn Discrete-Time Optimality Conditions for Pseudospectral Methodsen_US
dc.typeConference Paperen_US
dc.contributor.corporateOptimal Guidance and Control Laboratory
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.corporateThe American Institute of Aeronautics and Astronautics (AIAA)
dc.contributor.departmentApplied Mathematics
dc.subject.authorspace trajectory optimizationen_US
dc.subject.authorPseudospectral (PS) methodsen_US
dc.subject.authorGauss-Lobatto PSen_US
dc.subject.authorinfinite-horizon optimal control problemsen_US
dc.subject.authorCovector Mapping Principleen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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