AIAA Guidance, Navigation, and Control Conference 2009 Help me understand this report
Lisa Pathfinder Mission: Attitude and Orbit Control Based on Micropropulsion Systems
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“…The actuator's specifications are the main drivers of the MPACS design [2]. The MPACS phase is composed of two modes: Sun Acquisition and Safe Mode (MSAM), plus Normal Mode (MNM).…”
Section: Micro-propulsion Aocs Requirements and Design Driversmentioning
confidence: 99%
“…The actuator's specifications are the main drivers of the MPACS design [2]. The MPACS phase is composed of two modes: Sun Acquisition and Safe Mode (MSAM), plus Normal Mode (MNM).…”
Section: Micro-propulsion Aocs Requirements and Design Driversmentioning
confidence: 99%
“…This phase • Micro-Propulsion Attitude Control System (MPACS) takes over once the separation of the SCM has occurred and is based on the FEEP propulsion system. MPACS controls the spacecraft while on station and in between the science operation phases [2].…”
Section: Lisa Pathfinder Aocs Overviewmentioning
confidence: 99%
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