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UAV Performance Improvement Using Integrated Analysis and Design Optimization Technology

통합 해석 및 설계 최적화 기술을 이용한 무인기 성능 향상 연구

  • 김지민 (건국대학교 항공우주정보시스템공학과) ;
  • 누엔 반 (건국대학교 항공우주정보시스템공학과) ;
  • 서정일 (건국대학교 항공우주정보시스템공학과) ;
  • 티안 막심 (건국대학교 항공우주정보시스템공학과) ;
  • 이재우 (건국대학교 항공우주정보시스템공학과) ;
  • 김상호 (건국대학교 항공우주정보시스템공학과)
  • Received : 2013.01.07
  • Accepted : 2013.03.15
  • Published : 2013.03.31

Abstract

This paper describes the design optimization of Unmanned Aerial Vehicles(UAVs). An optimization framework has been developed and implemented for the conceptual design of UAVs. An integrated design analysis program was developed with several analysis modules such as propulsion, performance, mission, weight, and stability and control. A UAV configuration design optimization was performed by implementing the integrated analysis to enhance the endurance of UAVs. A SQP optimizer was utilized to build an optimization module for this program and sensitivity analysis was performed to determine the trends of shape variables for developing optimization objective. In conclusion, the results indicate that the resulting optimized UAVs configurations show performance improvements over the baseline design and reliable analysis results.

Keywords

References

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