Orbit Injection Error Mitigation by Time-Differenced GPS Carrier Phase Observables-Aided Inertial Navigation
AIAA Guidance, Navigation, and Control Conference
2017-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Adaptive Interplanetary Navigation Using Differenced Range Observables
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|Doubly-Differenced Measurements for Orbit Determinations
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