Optimal control theory with aerospace applications / Joseph Z. Ben-Asher.

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Bibliographic Details
Superior document:AIAA education series
:
TeilnehmendeR:
Year of Publication:2010
Language:English
Series:AIAA education series.
Online Access:
Physical Description:xvii, 262 p. :; ill.
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100 1 |a Ben-Asher, Joseph Z.,  |d 1955- 
245 1 0 |a Optimal control theory with aerospace applications  |h [electronic resource] /  |c Joseph Z. Ben-Asher. 
260 |a Reston, Va. :  |b American Institute of Aeronautics and Astronautics, Inc.,  |c c2010. 
300 |a xvii, 262 p. :  |b ill. 
490 1 |a AIAA education series 
504 |a Includes bibliographical references and index. 
505 0 |a Historical background -- Ordinary minimum problems : from the beginning of calculus to Kuhn-Tucker -- Calculus of variations : from Bernoulli to Bliss -- Minimum principle of Pontryagin and Hestenes -- Application of the Jacobi test in optimal control and neighboring extremals -- Numerical techniques for the optimal control problem -- Singular perturbation technique and its application to air-to-space interception -- Application to aircraft performance : Rutowski and Kaiser's techniques and more -- Application to rocket performance : the Goddard problem -- Application to missile guidance : proportional navigation -- Application to time-optimal rotational maneuvers of flexible spacecraft. 
533 |a Electronic reproduction. Ann Arbor, MI : ProQuest, 2015. Available via World Wide Web. Access may be limited to ProQuest affiliated libraries. 
650 0 |a Automatic pilot (Airplanes) 
650 0 |a Flight control. 
650 0 |a Guided missiles  |x Control systems. 
655 4 |a Electronic books. 
710 2 |a ProQuest (Firm) 
830 0 |a AIAA education series. 
856 4 0 |u https://ebookcentral.proquest.com/lib/oeawat/detail.action?docID=3111516  |z Click to View