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- W2619452089 abstract "Installation dynamics, optimal class of thruster propulsion, specific impulse thrust for reignitable fuel motors to regulate pointing error is given for satellite parked in transfer orbit for geosynchronous (e.g. the Indian National Satellite, INSAT-1B), sunsynchronous (e.g. the Indian Earth Resource Satellite, IRS-1) orbits. Filter dynamics for slow/fast terrestrial system are obtained. Design for inter satellite link server to maximize drop outlets is given. Extension of commutative Rings for coordinated control/communication of targets with predetermined signature in global and protected environment is given. Visibility model of flexible structure space monitoring station with associated space coordinate system is given. Technique proposed is applied for information acquisition synchronization of inertial targets. Design of long range navigation in projective space and robust controller AAFM auto pilot system for hybrid reliability is given." @default.
- W2619452089 created "2017-06-05" @default.
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- W2619452089 date "2000-07-01" @default.
- W2619452089 modified "2023-09-25" @default.
- W2619452089 title "Launch - Installation and Propulsion Control Satellite Locator System" @default.
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- W2619452089 doi "https://doi.org/10.1016/s1474-6670(17)39621-0" @default.
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