Accession Number:

ADA482873

Title:

System Analysis and Design of a Low-Cost Micromechanical Seeker System

Descriptive Note:

Master's thesis

Corporate Author:

MASSACHUSETTS INST OF TECH CAMBRIDGE

Personal Author(s):

Report Date:

2008-06-01

Pagination or Media Count:

141.0

Abstract:

Precision guided targeting systems have been in use by the U.S. military for the last half-century. The desire for high targeting accuracies while maintaining minimal collateral damage has driven the implementation of guidance systems on a myriad of different platforms. Current seeker systems using global positioning system GPS-aided technology offer good accuracy, but are limited by an adversarys signal jamming capabilities and the dynamic nature of the military target environment. Furthermore, ultra-accurate inertial measurement units IMU that serve as stand-alone guidance systems are very expensive and offer no terminal guidance enhancement. As a result, it is cost prohibitive to equip some platforms with precision guidance capability. The demand for high accuracy at low cost has prompted substantial recent development of micro-electromechanical systems MEMS IMU s and optical focal plane arrays FPA. The resulting decreasing device size and production costs coupled with higher unit performance have created opportunities for implementing seeker-enabled systems on platforms previously deemed impractical. As a result, the author proposes a design methodology to develop a low-cost system while satisfying stringent performance requirements. The methodology is developed within the context of a strap-down seeker system for tactical applications. The design tenets of the optical sensor, the inertial sensor, and projectile flight dynamics were analyzed in-depth for the specific scenario. The results of each analysis were combined to formulate a proposed system. The system was then modeled to produce system miss distance estimates for differing engagement situations. The system demonstrated 3 sigma miss distance estimates that were less than the maximum allowable error in each case. The system cost was tabulated and a production price was approximated.

Subject Categories:

  • Economics and Cost Analysis
  • Navigation and Guidance
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE