Optimal control theory with aerospace applications
Ben-Asher, Joseph Z., 1955-
Optimal control theory with aerospace applications [electronic resource] / Joseph Z. Ben-Asher. - Reston, Va. : American Institute of Aeronautics and Astronautics, Inc., c2010. - xvii, 262 p. : ill. - AIAA education series . - AIAA education series. .
Includes bibliographical references and index.
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.
Electronic reproduction.
Palo Alto, Calif. :
ebrary,
2013.
Available via World Wide Web.
Access may be limited to ebrary affiliated libraries.
Automatic pilot (Airplanes)
Flight control.
Guided missiles--Control systems.
Electronic books.
TL589.4 / .B46 2010eb
629.132/6
Optimal control theory with aerospace applications [electronic resource] / Joseph Z. Ben-Asher. - Reston, Va. : American Institute of Aeronautics and Astronautics, Inc., c2010. - xvii, 262 p. : ill. - AIAA education series . - AIAA education series. .
Includes bibliographical references and index.
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.
Electronic reproduction.
Palo Alto, Calif. :
ebrary,
2013.
Available via World Wide Web.
Access may be limited to ebrary affiliated libraries.
Automatic pilot (Airplanes)
Flight control.
Guided missiles--Control systems.
Electronic books.
TL589.4 / .B46 2010eb
629.132/6