Ultra-tightly coupled global navigation satellite system...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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C701S004000, C701S226000, C342S357490, C342S358000

Reexamination Certificate

active

07668629

ABSTRACT:
A GNSS ultra-tight coupling (UTC) receiver architecture applicable to space borne orbit platforms is described. A receiver in accordance with this architecture retains the rotational motion sensors typically found in an inertial measurement unit (IMU) of a conventional UTC receiver, but replaces the IMU accelerometer sensors with precise orbital dynamics models to predict the translational motion of the platform center of gravity (CG). Drag and radiation pressure may be modeled as well. The various models can be implemented in software. The IMU rotational sensors are retained for compensation of the GNSS antenna lever arm effect due to platform rotation.

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patent: 2006/0074558 (2006-04-01), Williamson et al.
patent: 1857833 (2007-11-01), None
J.A. Tekawy, Precision Spacecraft Attitude Estimators Using an Optical Payload Pointing System, Journal of Spacecraft and Rockets, vol. 35, No. 4, Jul.-Aug. 1998, pp. 480-486.

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