Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy

Orbit Model Analysis And Dynamic Filter Compensation For Onboard Autonomy

Orbit of a spacecraft in three dimensional Inertial Reference Frame is in general represented by a standard set of six parameters like Keplerian Orbital Elements namely semimajor axis, eccentricity, inclination, argument of perigee, right ascension of ascending node, and true anomaly....

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Bibliographic Details
Main Author: Akila, S
Other Authors: Ghosh, M K
Language:en_US
Published: 2009
Subjects:
Orbit Models
Spacecraft Orbits
Dynamic Filters
Orbit Dynamics
Orbit Determination (OD)
Orbit Propagation
Kalman Filter
Dynamics Filter Compensation (DFC)
Astronautics
Online Access:http://hdl.handle.net/2005/398

Internet

http://hdl.handle.net/2005/398

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