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OverviewFull Product DetailsAuthor: John E. Prussing (Professor Emeritus of Aerospace Engineering, Professor Emeritus of Aerospace Engineering, University of Illinois)Publisher: Oxford University Press Imprint: Oxford University Press Dimensions: Width: 15.70cm , Height: 0.80cm , Length: 23.50cm Weight: 0.276kg ISBN: 9780198811114ISBN 10: 019881111 Pages: 160 Publication Date: 21 December 2017 Audience: College/higher education , Undergraduate Format: Paperback Publisher's Status: Active Availability: To order ![]() Stock availability from the supplier is unknown. We will order it for you and ship this item to you once it is received by us. Table of Contents1: Parameter Optimization 2: Rocket Trajectories 3: Optimal Control Theory 4: Optimal Trajectories 5: Improving a Nonoptimal Impulsive Trajectories 6: Continuous-Thrust Trajectories 7: Cooperative Rendezvous 8: Second Order Conditions A: Lagrange Multiplier Interpretation B: Hohmann Transfer C: Optimal Impulsive Linear Systems D: Linear System Theory E: Maximum Range Using Continuous Thrust in a Uniform Gravitational Field F: Quadratic Forms G: Simple Conjugate Point ExampleReviewsAuthor InformationJohn Prussing is Professor Emeritus of Aerospace Engineering at the University of Illnois at Urbana-Champaign. He holds a SB, SM and a ScD in 1967 in aerospace engineering all from MIT, and served as professor of aerospace engineering between 1969 and 2007, and continues to teach part time, including short courses at NASA. He has published over 80 articles and has authored/co-authored three books. Tab Content 6Author Website:Countries AvailableAll regions |