IRNSS Satellite Parameter Estimation using Combination Strategy

§ INDIAN SPACE RESEARCH ORGANISATION INDIAN SPACE RESEARCH ORGANISATION

Send Message

To: Author

IRNSS Satellite Parameter Estimation using Combination Strategy

Article Fingerprint

ReserarchID

V978W

IRNSS Satellite Parameter Estimation using Combination Strategy Banner

Key Research Insights

Synthesized scholarly intelligence & interactive research assistant
  • English
  • Afrikaans
  • Albanian
  • Amharic
  • Arabic
  • Armenian
  • Azerbaijani
  • Basque
  • Belarusian
  • Bengali
  • Bosnian
  • Bulgarian
  • Catalan
  • Cebuano
  • Chichewa
  • Chinese (Simplified)
  • Chinese (Traditional)
  • Corsican
  • Croatian
  • Czech
  • Danish
  • Dutch
  • Esperanto
  • Estonian
  • Filipino
  • Finnish
  • French
  • Frisian
  • Galician
  • Georgian
  • German
  • Greek
  • Gujarati
  • Haitian Creole
  • Hausa
  • Hawaiian
  • Hebrew
  • Hindi
  • Hmong
  • Hungarian
  • Icelandic
  • Igbo
  • Indonesian
  • Irish
  • Italian
  • Japanese
  • Javanese
  • Kannada
  • Kazakh
  • Khmer
  • Korean
  • Kurdish (Kurmanji)
  • Kyrgyz
  • Lao
  • Latin
  • Latvian
  • Lithuanian
  • Luxembourgish
  • Macedonian
  • Malagasy
  • Malay
  • Malayalam
  • Maltese
  • Maori
  • Marathi
  • Mongolian
  • Myanmar (Burmese)
  • Nepali
  • Norwegian
  • Pashto
  • Persian
  • Polish
  • Portuguese
  • Punjabi
  • Romanian
  • Russian
  • Samoan
  • Scots Gaelic
  • Serbian
  • Sesotho
  • Shona
  • Sindhi
  • Sinhala
  • Slovak
  • Slovenian
  • Somali
  • Spanish
  • Sundanese
  • Swahili
  • Swedish
  • Tajik
  • Tamil
  • Telugu
  • Thai
  • Turkish
  • Ukrainian
  • Urdu
  • Uzbek
  • Vietnamese
  • Welsh
  • Xhosa
  • Yiddish
  • Yoruba
  • Zulu
Reading Preferences
Font Size
Line Spacing
Background

Abstract

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).

References

11 Cites in Article
  1. IRNSS Comprehensive Review Document.
  2. M Athans,P Falb (1966). Optimal Contro.
  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.

How to Cite This Article

Babu R, Prasanta Mula, S C Ratnakara. 2015. "IRNSS Satellite Parameter Estimation using Combination Strategy". Global Journal of Science Frontier Research - A: Physics & Space Science GJSFR-A Volume 15 (GJSFR Volume 15 Issue A3).

Download Citation

Journal Specifications

Crossref Journal DOI 10.17406/GJSFR

Print ISSN 0975-5896

e-ISSN 2249-4626

Keywords
Classification
GJSFR-A Classification FOR Code: 290207
Version of record

v1.2

Issue date
June 30, 2015

Language
English
Experiance in AR

Explore published articles in an immersive Augmented Reality environment. Our platform converts research papers into interactive 3D books, allowing readers to view and interact with content using AR and VR compatible devices.

Read in 3D

Your published article is automatically converted into a realistic 3D book. Flip through pages and read research papers in a more engaging and interactive format.

Article Matrices
Total Views: 1.5K
Total Downloads: 98
All Trends

Request Access

Please fill out the form below to request access to this research paper. Your request will be reviewed by the editorial or author team.
X

This is the heading

Lorem ipsum dolor sit amet, consectetur adipiscing elit. Ut elit tellus, luctus nec ullamcorper mattis, pulvinar dapibus leo.

High-quality academic research articles on global topics and journals.

IRNSS Satellite Parameter Estimation using Combination Strategy

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