Integration of GPS and baro-inertial loop aided strapdown ins and radar altimeter

IETE Journal of Research

Volumn 43, Issue 5, 1997, Pages 383-390

  Rao, K Deergha ^a  

^a OSMANIA UNIVERSITY   (India)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; ERROR ANALYSIS; INERTIAL NAVIGATION SYSTEMS; KALMAN FILTERING; MATHEMATICAL MODELS; MEASUREMENT ERRORS; RADAR;

BARO INERTIAL LOOP AIDED STRAPDOWN INERTIAL NAVIGATION SYSTEMS (INS); RADAR ALTIMETERS;

GLOBAL POSITIONING SYSTEM;

EID: 0031223789     PISSN: 03772063     EISSN: 0974780X     Source Type: Journal    
DOI: 10.1080/03772063.1997.11416005     Document Type: Article

References (6)

1. B, David & F, Michael, Integration of GPS and Strapdown Inertial Subsystems into a Single Unit, Navigation, Journal of the Institute of Navigation, vol 34, no 2, pp 140–159, 1987.
2. M, Shibata, Error Analysis Strapdown Inertial Navigation Using Quaternions, Journal of Guidance, Control and Dynamics, vol 9, no 3, pp 379–381, May-June 1986.
3. D H, Titherton & J L, Weston. Strapdown Inertial Navigation Technology, Peter Peregrinus Ltd, London 1997.
4. E J, Lefferts, F L, Markley & M D, Shuster, Kalman Filtering for Spacecraft Attitude Estimation, Journal of Guidance, Control and Dynamics, vol 5. no 5, pp 417–429, Sept-Oct 1982.
5. Appendix ‘K’ of RTCA Doc 208. Minimum Operational Standards for Airborne Supplemental Navigation Equipment Using GPS.
6. Dang G, Tuckness, Future Lunar Landing Navigation Schemes, With Emphasis on Precision Landings, Navigation, Journal of the Institute of Navigation, vol 41, pp 215–227, Summer, 1994.