Optimized Guidance of a Supersonic Projectile Using Pin Based Actuators-Reference-Cited by-同舟云学术

Optimized Guidance of a Supersonic Projectile Using Pin Based Actuators

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Massey Kevin¹,Guthrie Kevin¹,Silton Sidra²

Affiliation:

1. Georgia Tech Research Institute

2. U.S. Army Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4966

Reference7 articles.

1. Kandebo,StanleyW."NewPowerplantKeytoMissileDemonstrator,"AviationWeek,Sept.2,2002.

2. Low cost, high G, micro electro-mechanical systems (MEMS), inertial measurements unit (IMU) program

3. Frost, G. W., and Costello, M. F. "Control Authority of a Projectile Equipped With an Internal UnbalancedPart,"ArmyResearchLabReport,ARL-CR-555,November2004.

4. Massey, K. C., McMichael, J., Warnock, T., and Hay, F. "Design and Wind Tunnel Testing of Guidance Pinsfor SupersonicProjectiles,"25thArmyScienceConference,Dec.2004.

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