Optimal Spacecraft Trajectories
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59 718 Ft (56 875 Ft + 5% VAT)
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59 718 Ft
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Product details:
- Publisher OUP Oxford
- Date of Publication 21 December 2017
- ISBN 9780198811084
- Binding Hardback
- No. of pages152 pages
- Size 237x164x14 mm
- Weight 410 g
- Language English 0
Categories
Short description:
A tetxtbook on the theory and applications of optimal spacecraft trajectories
MoreLong description:
This graduate textbook on optimal spacecraft trajectories demonstrates the theory and applications of using the minimum amount of propellant possible to reach a target destination. The author aims to produce the only comprehensive treatment of various aspects of this topic. It includes problems at the ends of the chapters and some of the appendices. But it is also suitable as a scholarly reference book as it includes recent research from the author and his colleagues.
MoreTable of Contents:
Parameter Optimization
Rocket Trajectories
Optimal Control Theory
Optimal Trajectories
Improving a Nonoptimal Impulsive Trajectories
Continuous-Thrust Trajectories
Cooperative Rendezvous
Second Order Conditions
Lagrange Multiplier Interpretation
Hohmann Transfer
Optimal Impulsive Linear Systems
Linear System Theory
Maximum Range Using Continuous Thrust in a Uniform Gravitational Field
Quadratic Forms
Simple Conjugate Point Example
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