Spacecraft Guidance Systems
Spacecraft Guidance Systems
- New search for: Tewari, Ashish
- New search for: Tewari, Ashish
This chapter contains sections titled:
Introduction
Orbital Mechanics
Spacecraft Terminal Guidance
General Orbital Plant for Tracking Guidance
Planar Orbital Regulation
Optimal Non‐planar Orbital Regulation
Summary
Exercises
References
Document information
Spacecraft Guidance Systems
2011-07-15
59 pages
Article/Chapter (Book)
Electronic Resource
English
spacecraft guidance systems , Battin's hypergeometric function method ‐ Lambert problem, using hypergeometric functions , small magnitude of perturbations ‐ atmospheric drag, modifying trajectory , space flight, more predictable ‐ than aircraft or rocket flight , tracking, nominal orbit ‐ with non‐planar acceleration inputs , two spherical body, relative motion ‐ mutual gravitational attraction, orbital mechanics , general orbital plant for tracking guidance ‐ desired orbit, in orbital perturbations , Lambert's problem, general 2PBVP ‐ from a two‐body orbital transfer , planar orbital regulation ‐ planar orbit control task, radial and circumferential thrusts , Hyperbolic Orbit, equivalent form of Kepler's equation ‐ hyperbolic anomaly, H
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