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On-Board Orbit Determination function, providing :

DIODE. On-Board Orbit Determination function, providing : satellite position/velocity (plus a quality assessment), TAI time-tagging (plus a quality assessment), ancillary products (next beacon, expected Doppler, …), elaborated on-board and in real-time every ten seconds.

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On-Board Orbit Determination function, providing :

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  1. DIODE • On-Board Orbit Determination function, providing : • satellite position/velocity (plus a quality assessment), • TAI time-tagging (plus a quality assessment), • ancillary products (next beacon, expected Doppler, …), • elaborated on-board and in real-time every ten seconds. • Products are useful for : • platform and payload, • ground processing of the data (images, altimetry, …), • DORIS receiver (self-programming and reduction of Doppler tolerances).

  2. DIODE / SPOT4 • A probatory experiment ... • validation of the concept (routine filter only), • limited amount of memory on a dedicated card, • software completed in June 1995. • … but already with users of the products : • POAM (NRL, for optical terminal pointing), • SPOT IMAGE (ground immediate and precise rectification), • VEGETATION (idem), • DIODE monitoring and R&D evolutions.

  3. DIODE / SPOT4 : main features • Only the routine Kalman filter : • prediction/correction every ten seconds, • state vector : position, velocity, frequency & tropospheric biases. • Extrapolation model : • Runge-Kutta numerical integration (Gill), • force model = 15x15 E.G.F., nominal thrust accel. • Measurement model : • ionospheric error (two-frequency measurement), • on-board clock estimated with Master Beacons.

  4. DIODE/SPOT4 on-orbit results

  5. DIODE / SPOT4 conclusions • After more than two years : • accuracy = a few meters RMS, • availability > 99.6% (unavailable 62h over 750 days), • meet specifications (200 m MAX) > 99.7%), • good behaviour during manœuvers (see paper). • users of the products : • POAM several times a day (near poles), • SPOT IMAGE : DIODE is the nominal source for image positionning, • VEGETATION (permanent since July 1999).

  6. DIODE / Jason-1 • Complete mission, including : • improved dynamical model, • improved autonomy : • self-initialisation (« lost in space »), • self-programming of the DORIS receiver, • TAI (or TUC) time-tagging of external events. • Users of the products : • quick-look processing of altimetric data, • possible use by the platform, • and by (SPOT5) the ground Control Center.

  7. DIODE / Jason-1 : main evolutions • New functionnalities : • self-initialisation algorithm (4 passes, two filters), • receiver programming (prediction of the next-to-come beacon, optimal choice, Doppler shift). • Improved models : • adjusted : Earth pole coordinates, Hill accelerations, thrust accelerations, • force model = 40x40 optimised E.G.F., moon&sun attractions, solar pressure (box&wings), air drag, • improved quality assessments.

  8. DIODE/TOPEX ground results • (64 bits SPARC processor)

  9. DIODE / Jason-1 objectives • Performances : • routine accuracy : goal = 1m RMS 3D, a few centimeters radial RMS (between 5 and 14), • self-initialisation mean time =1 hour, • time determination (goal= a few microseconds), • operationnal use of the self-programming mode. • Availability : • goal = 100 % .

  10. DIODE future perspectives • Already planned : Jason-1, SPOT5, ENVISAT, • T.B.C : PLEIADES (SPOT follow-on), • On Skybridge, DORIS/DIODE has been evaluated as technically acceptable, • Currently under study : • ISS (ACES), ATV, CRYOSAT, ALTIKA, • Navigation dedicated DORIS receivers...

  11. DIODE/TOPEX cy 232 radial errors • (64 bits SPARC processor)

  12. DIODE/TOPEX radial errors • (64 bits SPARC processor)

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