Satellite Realtime Navigation

Applications
Title	Satellite Realtime Navigation
Author(s)	GMV.
Level	Medium
Year of Publication	2011

From the very beginning it was realized that these systems could also be used for a wide range of scientific and other civil applications. New tracking methods that were not foreseen by the original developers of the systems, like carrier tracking, were proposed and, as soon as it was possible, successfully tested and used. One of the applications that was soon envisioned was the use of GPS for navigation of spacecraft. The first onboard receiver was installed and flown in a Landsat satellite even before the complete GPS constellation was deployed. Since that time, more receivers have been flown on satellites, at first as a demonstration of increasingly precise uses and now as the main operational means of navigation.

Application Architecture

For Satellite Realtime Navigation it is not usually possible to rely on post-processing algorithms and ground based station networks. For Low Earth Orbit spacecrafts kinematic point position solutions present a similar accuracy has terrestrial applications. This accuracy can be improved by using algorithms that incorporate a dynamic model of the spacecraft's orbit.

Application Characterization

Currently kinematic Point Position solutions can achieve a navigation accuracy of 10 m and 0.1 m/s for GNSS receivers on Low Earth Orbit without further optimizations. This level of navigation accuracy is considered adequate for attitude and orbit control systems. Meter level accuracy can be achieved using onboard Kalman filters and algorithms that take into account the dynamic model of the orbit.

Experiments with the Proba-2 satellite show that 1-2 m positioning accuracy could be achieved using onboard advanced real-time navigation filters.

Application Examples

• ATV - Automated Transfer Vehicle - Expendable, unmanned resupply spacecraft developed by the European Space Agency. GPS and a star tracker is used to automatically rendezvous with the International Space Station and at a distance of 249 m, the ATV computers use videometer and telegoniometer data for final approach and docking manoeuvres.
• Proba-2 - The Proba satellites are part of ESA’s In-orbit Technology Demonstration Programme, missions dedicated to the demonstration of innovative technologies. Proba-2 incorporates two experimental GPS receivers for demonstration of Satellite Realtime Navigation and Precise Orbit Determination.