Global ETD Search

1	A multi-loop guidance scheme using singular perturbation and linear quadratic regulator techniques simultaneously / Bushong, Philip Merton, January 1991 (has links) Thesis (Ph. D.)--Virginia Polytechnic Institute and State University, 1991. / Vita. Abstract. Includes bibliographical references (leaves 68-71). Also available via the Internet. Guidance systems (Flight)
2	PRECOMPUTED STATE DEPENDENT DIGITAL CONTROL OF A NUCLEAR ROCKET ENGINE Johnson, Morris Ray, 1937- January 1972 (has links) No description available. Guidance systems (Flight) Automatic control.
3	Design techniques for a class of multirate sampled data control systems Flowers, David Carl 08 1900 (has links) No description available. Feedback control systems Guidance systems (Flight)
4	Development, modeling, and simulation of a nano aerial vehicle using empirical data Davenport, Wyatt Emery, January 2007 (has links) (PDF) Thesis (M.S.)--University of Missouri--Rolla, 2007. / Vita. The entire thesis text is included in file. Title from title screen of thesis/dissertation PDF file (viewed January 28, 2008) Includes bibliographical references (p. 83-84).
5	Integration of local area augmentation system and inertial navigation system for aircraft surface movement guidance Marti, Lukas Michael. January 2000 (has links) Thesis (M.S.)--Ohio University, August, 2000. / Title from PDF t.p.
6	Linearised optimal control and application to a gliding projectile / Jepps, G. January 1980 (has links) (PDF) Thesis (M.Eng.Sc.) - Dept. of Electrical and Electronic Engineering, University of Adelaide, 1983. / AR-003-687. Originally his Thesis (M.Eng.Sc.) - Dept. of Electrical and Electronic Engineering, University of Adelaide, 1980. Photostat. Includes bibliographical references (p. 66-67).
7	Guidance, navigation, and control for munitions / Ilg, Mark Dean. Chang, Bor-Chin. January 2008 (has links) Thesis (Ph.D.)--Drexel University, 2008. / Includes abstract and vita. Includes bibliographical references (leaves 120-126).
8	A study of observability-enhanced guidance systems / by George Estandy Hassoun. Hassoun, George Estandy January 1995 (has links) Erratum pasted on front fly leaf. / Bibliography: leaves 204-214. / xxi, 214 leaves : ill. ; 30 cm. / Title page, contents and abstract only. The complete thesis in print form is available from the University Library. / This thesis investigates a novel guidance law dubbed "observable proportional navigation". Two distinct forms of this guidance law are considered, based on the nature of the associated noise and state estimator. Closed-form solutions are given and necessary limits on the co-efficient of observability are determined. Both forms of the new law are applied to a two-dimensional missile-target bearing-only-measurement problem. / Thesis (Ph.D.)--University of Adelaide, Dept. of Electrical and Electronic Engineering, 1995 Guidance systems (Flight) Observers (Control theory) Proportional navigation.
9	Development of an attitude heading reference system for an airship / Bijker, Johan. January 2006 (has links) Thesis (MScIng)--University of Stellenbosch, 2006. / Bibliography. Also available via the Internet.
10	UAV guidance control laws for autonomous coordinated tracking of a moving ground target / Wise, Richard, January 2007 (has links) Thesis (Ph. D.)--University of Washington, 2007. / Vita. Includes bibliographical references (p. 111-114).

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