Testing of ultra-tightly-coupled GPS operation using a precision GPS/inertial simulator

Proceedings of the 18th International Technical Meeting of the Satellite Division of The Institute of Navigation, ION GNSS 2005

Volumn 2005, Issue , 2005, Pages 439-447

  Brown, Alison ^a,b   Nguyen, Dien ^a,c   Lu, Yan ^a   Wang, Chaochao ^a  

^a NAVSYS Corporation   (United States)

^b SIDNEY SUSSEX COLLEGE   (United Kingdom)

^c UNIVERSITY OF COLORADO   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANTI-JAM GPS RECEIVERS; RESIDUAL CARRIER ERROR; ULTRA-TIGHTLY-COUPLED (UTC); UTC SIGNAL PROCESSING;

COMPUTER SIMULATION; JAMMING; ROBUSTNESS (CONTROL SYSTEMS); SIGNAL PROCESSING; SIGNAL RECEIVERS;

GLOBAL POSITIONING SYSTEM;

EID: 33646546034     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. P. Bruner, R. Breslau, "Use of Inertial Reference Data to Support Differential GPS For Carrier Landing," Proceedings of ION 57th Annual Meeting 2001, Albuquerque, New Mexico, June 2001
2. A. Brown and B. Mathews, "GPS Multipath Mitigation Using a Three Dimensional Phased Array:, Proceedings of ION GNSS 2005, Long Beach, California, September 2005
3. http://waas.stanford.edu/research/jpals.htm
4. InterNav Modular GPS/Inertial Software
5. http://www.mathworks.com/
6. STANAG 4572 - Open System Architecture Interface to Enable Simulator Laboratory Test of Integrated Global Positioning System/Inertial Navigation Equipment, Version G
7. NAVSYS NIM Timestamp Board Specification and ICD, NAVSYS Document No. Timestamp Board-04-001, Rev 6, January 30, 2005
8. "Minimum Operational Performance Standards for Global Positioning System/Wide Area Augmentation System Airborne Equipment," RTCA/DO-229C, November 28, 2001.