Guidance, navigation and control without gyros: A gun-launched munition concept

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Ohlmeyer, Ernest J ^a   Fraysse, John W ^a   Pepitone, Thomas R ^b  

^a NAVAL SURFACE WARFARE CENTER   (United States)

^b Aerospace Technology Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELEROMETERS; COSTS; FLIGHT CONTROL SYSTEMS; GYROSCOPES; INERTIAL NAVIGATION SYSTEMS;

AUTONOMOUS NAVAL SUPPORT ROUNDS; CLOSED-LOOP PERFORMANCE; GUIDANCE , NAVIGATION AND CONTROLS; GUIDED PROJECTILES; INTEGRATED TERMINALS; STRAPDOWN INERTIAL MEASUREMENT UNITS; SYSTEM IMPLEMENTATION; THREE-AXIS MAGNETOMETER;

COMMERCIAL OFF-THE-SHELF;

EID: 85088721287     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-5025     Document Type: Conference Paper

References (3)

1. Fraysse, J.W., "ANSR System Definition" PowerPoint Presentation, NSWCDD, Dahlgren, VA, March, 2000.
2. Ohlmeyer, E. J., Pepitone, T. R., Miller, B. L., "Assessment of Integrated GPS/INS for the EX-171 Ex -tended Range Guided Munition," Proceedings of AIAA Guidance, Navigation, and Control Conference, Boston, MA, Aug. 10-12, 1998, pp. 1374-1389.
3. Murphy, C. H., Free Flight Motion of Symmetric Missiles, BRL Report 1216, U. S. Army Ballistics Research Laboratory, Aberdeen Proving Grounds, MD, July, 1963.