IRNSS Satellite Parameter Estimation using Combination Strategy

1
Babu R
Babu R
2
Prasanta Mula
Prasanta Mula
3
S C Ratnakara
S C Ratnakara
1 INDIAN SPACE RESEARCH ORGANISATION

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Indian regional Navigation Satellite system (IRNSS) is going to be an independent, indigenous navigation satellite system fully controlled by India, planned by ISRO. A system was designed of regional navigation satellite constellation, as an alternate to GPS constellation, for providing space based navigation support to various land, sea and air navigation users over the Indian region. The proposed IRNSS constellation consists of 7 satellites (3 in GEO and 4 in inclined GSO with 29 deg inclination). The continuous visibility of GEO and GSO satellites for near-equator regions provides a promising alternative for regional navigation. The Signal In Space (SIS) broadcasts satellite ephemeris in quasi keplarian elements and satellite clock coefficients which forms the primary navigation parameters generated from navigation software located at INC (ISRO Navigation Centre), bylalu, India. The determination of these parameters is performed by two types of technique, batch least square (BLS) and Extended Kalman Filter (EKF).

11 Cites in Articles

References

  1. IRNSS Comprehensive Review Document.
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  3. A Gelb (1966). Applied Optimal Estimation.
  4. (2007). Unknown Title.
  5. James R Wright (2002). Optimal Orbit Determination.
  6. R Kalman (1960). A New Approach to Linear Filtering and Prediction Problems.
  7. C Price (1968). An analysis of the divergence problem in the Kalman filter.
  8. Mark Psiaki (2005). Backward-Smoothing Extended Kalman Filter.
  9. S Sherma (1958). Non-mean-square error criteria.
  10. A Mohamed,K Schwarz (1999). Adaptive Kalman Filtering for INS/GPS.
  11. S Kavitha,Prasanta Mula,Manamohan Kamat,S Nirmala,Joel Manathara (2015). Extended Kalman filter-based precise orbit estimation of LEO satellites using GPS range measurements.

Funding

No external funding was declared for this work.

Conflict of Interest

The authors declare no conflict of interest.

Ethical Approval

No ethics committee approval was required for this article type.

Data Availability

Not applicable for this article.

Babu R. 2015. \u201cIRNSS Satellite Parameter Estimation using Combination Strategy\u201d. Global Journal of Science Frontier Research - A: Physics & Space Science GJSFR-A Volume 15 (GJSFR Volume 15 Issue A3): .

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GJSFR Volume 15 Issue A3
Pg. 87- 95
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Crossref Journal DOI 10.17406/GJSFR

Print ISSN 0975-5896

e-ISSN 2249-4626

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GJSFR-A Classification: FOR Code: 290207
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v1.2

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June 30, 2015

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English

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Indian regional Navigation Satellite system (IRNSS) is going to be an independent, indigenous navigation satellite system fully controlled by India, planned by ISRO. A system was designed of regional navigation satellite constellation, as an alternate to GPS constellation, for providing space based navigation support to various land, sea and air navigation users over the Indian region. The proposed IRNSS constellation consists of 7 satellites (3 in GEO and 4 in inclined GSO with 29 deg inclination). The continuous visibility of GEO and GSO satellites for near-equator regions provides a promising alternative for regional navigation. The Signal In Space (SIS) broadcasts satellite ephemeris in quasi keplarian elements and satellite clock coefficients which forms the primary navigation parameters generated from navigation software located at INC (ISRO Navigation Centre), bylalu, India. The determination of these parameters is performed by two types of technique, batch least square (BLS) and Extended Kalman Filter (EKF).

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IRNSS Satellite Parameter Estimation using Combination Strategy

Babu R
Babu R INDIAN SPACE RESEARCH ORGANISATION
Prasanta Mula
Prasanta Mula
S C Ratnakara
S C Ratnakara

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