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.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
