Assessment of a GPS guided spinning projectile using an accelerometer-only IMU

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 1, Issue , 2004, Pages 705-717

  Pamadi, Kishore B ^a,c   Ohlmeyer, Ernest J ^a,c   Pepitone, Thomas R ^b  

^a NAVAL SURFACE WARFARE CENTER   (United States)

^b Aerospace Technology Inc   (United States)

^c Engagement Systems Department   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUTONOMOUS NAVAL SUPPORT ROUND (ANSR); CIRCULAR ERROR PROBABLE (CER); COMMERCIAL OFF THE SHELF (COTS); INERTIAL NAVIGATION SYSTEM (INS);

ACCELEROMETERS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); LAUNCHING; NAVIGATION; PROJECTILES; ROCKETS; SYSTEMS ANALYSIS;

GLOBAL POSITIONING SYSTEM;

EID: 19644366176     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Fraysse, J., "ANSR System Definition", NAVSEA Dahlgren Power-point presentation, Sept. 2001.
2. Ohlmeyer, E. J., Fraysse J. W., Pepitone T. R., "Guidance, Navigation and Control without Gyros: A Gun Launched Munition Concept" AIAA Guidance, Navigation, and Control Conference, AIAA-2002-5025, Monterey, CA, Aug. 2002.
3. Ohlmeyer, E. J., Pepitone, T. R., Miller, B. L., "Assessment of Integrated GPS/INS for the EX-171 Extended Range Guided Munition," AIAA Guidance, Navigation, and Control Conference, AIAA-1998-4416, Boston, MA, Aug. 1998.
4. Zarchan, P., Tactical and Strategic Missile Guidance, 4th ed., Progress in Astronautics and Aerospace, 2002.
5. Murphy C. H., "Free Flight Motion of Symmetric Missiles", Ballistic Research Lab Report 1216, Aberdeen Proving Ground, MD., July 1963.
6. nd ed.