A high G, MEMS based, deeply integrated, INS/GPS, guidance, navigation and control flight management unit

Record - IEEE PLANS, Position Location and Navigation Symposium

Volumn 2006, Issue , 2006, Pages 772-794

  Buck, Timothy M ^a   Wilmot, Jason ^a   Cook, Michael J ^b  

^a HONEYWELL   (United States)

^b ROCKWELL COLLINS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEEPLY INTEGRATED GUIDANCE; FLIGHT MANAGEMENT UNIT (FMU); INTEGRATED GUIDANCE SYSTEMS; SELECTIVE AVAILABILITY ANTI-SPOOF MODULE (SAASM);

COMPUTER PROGRAMMING LANGUAGES; FLIGHT DYNAMICS; MILITARY APPLICATIONS; MISSILES; OPTICAL SENSORS; PROJECTILES;

GLOBAL POSITIONING SYSTEM;

EID: 33845583492     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/PLANS.2006.1650674     Document Type: Conference Paper

References (5)

1. W. Soehren, B. Schipper, and C. Lund, "A MEMS Based, Guidance, Navigation and Control Unit", PLANS 2002
2. R. Phillips and G. Schmidt, "GPS/INS Integration", AGARD MSP Lecture Series 1996
3. D. Carlucci, J. Cordes, and J. Hahn, "Fuze and Precision Armaments Directorate", AETC, U.S. Army ARDEC
4. Sennott 1994 patent "Navigation Receiver with Coupled Signal Processing Channels" - Honeywell/Rockwell obtained license
5. "Optimal Processing of GPS Signals," Copps, Geier, Fidler & Grundy, Navigation: Journal of the ION, Vol. 27, No. 3, Fall 1980