DocumentCode :
2462624
Title :
Low cost, high G, micro electro-mechanical systems (MEMS), inertial measurements unit (IMU) program
Author :
Warnasch, Albert ; Killen, Albert
Author_Institution :
U.S. Army TACOM-ARDEC, Picatinny Arsenal, NJ, USA
fYear :
2002
fDate :
2002
Firstpage :
299
Lastpage :
305
Abstract :
Precision guided munitions (PGMs) are critical to the Maneuver Battalion Commander´s success on future rapidly deployed battlefields. These PGMs will provide an increase in lethality, significantly improve survivability, reduce collateral damage, minimize non-combatant casualties, and decrease the logistics burden or increase the number of kills from the standard logistics load. PGMs all require inertial measurement sensors embodied in an IMU. Until now, they have been large, expensive, and could not readily survive the high G launch environments. MEMS technology provides inherent cost savings and size reduction and is ideal for application to navigation and control systems for small missiles and munitions. Using MEMS technology, gyroscopes, accelerometers and control electronics can readily be integrated to form a tightly packaged, low-cost, extremely small, high performance IMU suitable for munition, missile, and personnel guidance as well as other applications. This paper describes the current Army development underway and its partnership with industry to achieve the necessary requirements. The program goal is to survive a 20,000 g gun launch and meet a 1°/hr, 1/2 milli-g performance capability. The MEMS IMUs will significantly reduce the cost of precision-delivered missiles and munitions, as well as expand precision delivery capability to artillery ammunitions, and thus reduce the number of required rounds by more than 30% while meeting roughly 90% of the tactical weapons fleet navigational requirements.
Keywords :
accelerometers; gyroscopes; inertial navigation; microsensors; military equipment; missile guidance; packaging; reliability; Army development; IMU; MEMS IMU; MEMS inertial measurements unit program; accelerometers; artillery ammunitions; artillery round reduction; collateral damage; control electronics; cost savings; gun launch; gyroscopes; high G launch environments; inertial measurement sensors; lethality; logistics burden; maneuver battalion commander; micro electro-mechanical systems; missiles; munitions; navigation/control systems; noncombatant casualties; packaged IMU; performance capability; personnel guidance; precision guided munitions; precision-delivered missiles; precision-delivered munitions; rapidly deployed battlefields; size reduction; standard logistics load; survivability; tactical weapons fleet navigational requirements; Control systems; Costs; Gyroscopes; Logistics; Measurement units; Micromechanical devices; Missiles; Navigation; Size control; Weapons;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Position Location and Navigation Symposium, 2002 IEEE
Print_ISBN :
0-7803-7251-4
Type :
conf
DOI :
10.1109/PLANS.2002.998922
Filename :
998922
Link To Document :
بازگشت