Spacecraft Navigation and Guidance
Published on 10. December 2011
Book
Paperback/Softback
XIV, 181 pages
978-1-4471-1585-4 (ISBN)
Description
The analysis and computational techniques associated with the navigation and guidance of spacecraft are now in a mature state of development. However the documentation has remained dispersed throughout conference papers, journals, company and contract rep orts, making it difficult to get a true, comprehensive picture of the subject. This text brings together the body of literature with suitable attention to the necessary underlying mathematics and computational techniques. It covers in detail the necessary orbital mechanics, orbit determination with emphasis on the SRIF algorithm, gr avity assist manoeuvres and guidance, both ground-based and autonomous. Attention is paid to all phases of a space mission including launch and re-entry, and whether culminating in an earth satellite or a deep space mission to planets or primitive bodies. Software associated with the text is available free to the reader by means of the Internet server of the publisher. 'Spacecraft Navigation and Guidance' is an invaluable aid for all those working within astronautics, aeronautics, and control engineering in general.
More details
Series
Edition
Softcover reprint of the original 1st ed. 1998
Language
English
Place of publication
London
United Kingdom
Target group
Professional and scholarly
Research
Illustrations
XIV, 181 p.
Dimensions
Height: 235 mm
Width: 155 mm
Thickness: 11 mm
Weight
309 gr
ISBN-13
978-1-4471-1585-4 (9781447115854)
DOI
10.1007/978-1-4471-1583-0
Schweitzer Classification
Other editions
Additional editions
Maxwell Noton
Spacecraft Navigation and Guidance
Book
03/1998
Springer
€85.55
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Content
1. Orbital Mechanics.- 1.1 Introduction.- 1.2 The Two-Body Problem.- 1.3 Orbital Elements and Reference Axes.- 1.4 Time in Orbit.- 1.5 Lambert's Time of Flight Theorem.- 1.6 Orbital Manoeuvres.- 1.7 Patched Conies.- 1.8 Numerical Integration of Orbits.- 1.9 Software.- 2. The Launch Phase.- 2.1 Introduction.- 2.2 Propulsion.- 2.3 Launch Systems.- 2.4 Trajectory Dynamics.- 2.5 Computation of the Nominal Ascent Trajectory.- 2.6 A Computed Example: Ariane 4.- 2.7 Optimization of the Ascent.- 2.8 In-flight Guidance.- 2.9 The Guidance and Navigation System.- 2.10 Software.- 3. Earth Satellites: Perturbations and Manoeuvres.- 3.1 Introduction.- 3.2 Variation of the Orbital Elements.- 3.3 Gravitational Field of the Earth.- 3.4 Perturbations from the Sun and the Moon.- 3.5 Effect of Atmospheric Drag.- 3.6 Illustrative Computations of Perturbations.- 3.7 Correcting Low Earth Orbits.- 3.8 Geostationary Orbits.- 3.10 Software.- 4. Orbit Determination.- 4.1 Introduction.- 4.2 First Estimates of Orbits.- 4.3 Refinement of Orbits.- 4.4 Sequential Estimation.- 4.5 Software.- 5. Midcourse and Gravity Assist Manoeuvres.- 5.1 Introduction.- 5.2 Midcourse Manoeuvres.- 5.3 Gravity Assist Manoeuvres.- 5.4 Software.- 6. Low Thrust Missions.- 6.1 Introduction.- 6.2 Electric Propulsion.- 6.3 Optimization of Low Thrust Trajectories.- 6.4 Guidance on Low Thrust Trajectories.- 6.5 Software.- 7. Atmospheric Entry.- 7.1 Introduction.- 7.2 Flight Equations.- 7.3 Entry Corridors.- 7.4 Ballistic Entry with No Lift.- 7.5 Guided Entry using Lift.- 7.6 Software.- A. Appendices.- A.1 Perturbations from the Sun and Moon in Geostationary Orbit.- A.2 Perturbations due to Solar Pressure in Geostationary Orbit.- A.3 Angular Information from Doppler Tracking.- A.4 Ephemeris of the Sun.- A.5 Sequential UDCovariance Filter.- A.6 Global Positioning System.