Abstract: | A gun launched Inertial-GPS receiver program was initiated by NSWC Dahlgren. An inertial sensor is being developed under this program which will withstand the high shock and rotational g’s ofthese munitions. The sensor is a micromachined silicon sensor, in a multisensor conftguration, required to meet the aggressive cost target of less than $3,000. The paper describes this inertial sensor and GPSRnertial architecture for minimized cost. A test program for the silicon sensor is described. System integration issues pertaining to “up fmding” or leveling ofthe reference Same in zero g field are also discussed. Finally, the packaging plan for this system is presented where MCMs with flipped chip bonded components with encapsulation are used to survive the 30,000 g set back shock. |
Published in: |
Proceedings of the 7th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS 1994) September 20 - 23, 1994 Salt Palace Convention Center Salt Lake City, UT |
Pages: | 477 - 482 |
Cite this article: | Singh, Mahendra, Fraysee, John, Kohli, Sanjai, "Silicon Inertial and GPS Guidance for Gun Launched Munitions," Proceedings of the 7th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS 1994), Salt Lake City, UT, September 1994, pp. 477-482. |
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