Military Applications

Case Study: Epoch-by-Epoch™ attitude determination at high-dynamics.

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Geodetics’ Vector™ software package was tested on a simulated maneuver employing an omni-directional antenna model. The maneuver and antenna model were programmed into the Guided Weapons Evaluation Facility (GWEF) satellite simulator.  The GWEF simulator is a model 2400 GPS Constellation Simulator from Interstate Electronics Corporation.  

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The simulated scenario consisted of a single stationary reference receiver and moving rigid platform upon which four antennas were mounted in a right-handed Cartesian coordinate system with inter-antenna spacing of 2 meters.

The simulation moved the rigid platform through two sets of maneuvers, one set occurring while the rigid platform was stationary, and the second occurring while the rigid platform was translating along a linear path.  During each maneuver set, the platform underwent three 360-degree rotations one rotation about each of the three axes of rotation (yaw, pitch and roll). Each rotation achieved a maximum of 9g’s.

The figure below compare Vector™ rigid platform attitude outputs with the ‘true’ attitude from the simulator for the maneuver.

The table below provides statistics (mean, standard deviation) for deviations from truth for the test.

 

 

 
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