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Suborbital Test of a Robotics-Based Method for In-Orbit Identification of Spacecraft Inertia Properties
PI: Ou Ma, New Mexico State University- 2 sRLV
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Design and Development of a Micro Satellite Attitude Control System
PI: Manoranjan Majji, State University of New York - Buffalo- 1 Parabolic
- 0 sRLV
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Fuel Optimal Large Divert Guidance for Planetary Pinpoint Landing (G-FOLD)
PI: Behcet Acikmese, NASA/Jet Propulsion Laboratory- 2 sRLV
Platform Type
< All Platform Types- sRLV (3)
Status
- Completed (3)