Attitude Ground System (AGS) for the Magnetospheric Multi-Scale (MMS) Mission
Use of GPS Tracking Data from Low Earth Flight Receiver to Determine Geocenter Location
Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle
Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle
Center of Mass Estimation for a Spinning Spacecraft Using Doppler Shift of the GPS Carrier Frequency
Center of Mass Estimation for a Spinning Spacecraft Using Doppler Shift of the GPS Carrier Frequency
Deployment Technology of a Heliogyro Solar Sail for Long Duration Propulsion
Orion Handling Qualities During ISS Rendezvous and Docking
A Highly Accurate Method for the Determination of Mass and Center of Mass of a Spacecraft
USML-1 Microgravity Glovebox Experiment No. 1 Passive Accelerometer System
Testing and Validation of the Dynamic Inertia Measurement Method