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Optimal spacecraft trajectories

Author: John E Prussing
Publisher: Oxford Oxford University Press 2018
Edition/Format:   Print book : English : First editionView all editions and formats
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A tetxtbook on the theory and applications of optimal spacecraft trajectories

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Document Type: Book
All Authors / Contributors: John E Prussing
ISBN: 9780198811114 019881111X 9780198811084 019881108X
OCLC Number: 1164617317
Notes: Literaturangaben.
Description: ix, 140 Seiten : Diagramme ; 24 cm
Contents: 1: Parameter Optimization2: Rocket Trajectories3: Optimal Control Theory4: Optimal Trajectories5: Improving a Nonoptimal Impulsive Trajectories6: Continuous-Thrust Trajectories7: Cooperative Rendezvous8: Second Order ConditionsA: Lagrange Multiplier InterpretationB: Hohmann TransferC: Optimal Impulsive Linear SystemsD: Linear System TheoryE: Maximum Range Using Continuous Thrust in a Uniform Gravitational FieldF: Quadratic FormsG: Simple Conjugate Point Example
Responsibility: John E. Prussing (Professor Emeritus, Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, Urbana, Illinois, USA).
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