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Captive Flight Test POD System Design for Effective Development in Weapon System

무기체계의 효과적인 개발을 위한 항공탑재시험용 POD 시스템 설계

  • Received : 2018.03.30
  • Accepted : 2018.06.20
  • Published : 2018.06.28

Abstract

Captive Flight Test (CFT) is one of the most important tests to acquire data when developing complex weapon systems. In this paper, we introduce the design and test result of our POD system for CFT. POD system uses POD set which consists of left and right POD. The exterior and mass properties of POD set are equal to those of fuel tank for aircraft so that we can omit Airworthiness Certification. Also, we adequately placed inner-equipments in order to acquire data including target image, navigation result and reference data to verify and analyse software algorithm. The POD system for CFT we developed is complex system as both mechanical and electronic factors are applied. As we repeatedly performed CFT, useful and various data for weapon development were acquired.

항공탑재시험은 복잡해지는 무기체계 개발과정에서 데이터 획득을 위해 수행하는 중요한 시험 중 하나이다. 본 논문은 무기체계 개발 과정중 수행하는 항공탑재시험용 POD 시스템에 대한 설계 내용 및 시험 결과를 소개한다. 항공탑재시험용 POD는 좌 우 2개의 POD가 설계 및 제작되었고 각각의 POD는 항공기 연료탱크와 동일한 외형과 질량특성을 갖도록 하여 감항인증 절차를 생략할 수 있도록 하였다. 또한 무기체계 개발에 필요한 표적 영상 데이터 계측, 항법 데이터 획득, 알고리듬 검증 및 분석에 필요한 기준 데이터를 획득할 수 있도록 구성품들을 적절하게 배치하였다. 항공탑재시험용 POD 시스템은 기계적, 전기적 요소들이 모두 반영된 복합적인 시스템이며 개발된 POD 시스템은 반복적으로 항공탑재시험에 사용되어 무기체계 개발에 필요한 다양한 데이터를 성공적으로 획득하였다.

Keywords

References

  1. S. M. Lee, S. C. Lee, H. S. Oh & D. Y. Sung. (2007). Test and Evaluation of Onboard Equipments for Guided Missile via Captive Flight Test. Journal of Korean Society for Aeronautical and Space Sciences, 35(1), 73-78. UCI : G704-000344.2007.35.1.006 https://doi.org/10.5139/JKSAS.2007.35.1.073
  2. S. M. Lee, S. C. Lee & Y. P. Lee. (2004, April). Test and Evaluation of Onboard Equipments for Guided Missile via Captive Flight Test. Spring Conference of Korean Society for Aeronautical and Space Sciences. (pp. 599-602). Seoul : KSAS.
  3. I. C. Park, W. Y. Heo, Y. H. Lee & S. Y. Jeong. (2016). Captive Flight Test System Configuration and Verification for Multi-mode Guidance Missile System. The Journal of Korea Institute of Military Science and Technology, 19(5), 606-612. DOI : 10.9766/KIMST.2016.19.5.606
  4. H. S. Yeom, J. H. Oh & D. Y. Sung. (2009). A Study on Technique of Development Test by an Aircraft Captive Flight Test in Weapon System. Journal of Korean Society for Aeronautical and Space Sciences, 37(10), 1010-1016. UCI : G704-000344.2009.37.10.010 https://doi.org/10.5139/JKSAS.2009.37.10.1010
  5. H. S. Yeom, J. H. Oh & M. S. Kim. (2010, November). Application of Captive Flight Test to Weapon System Development. Fall Conference of Korean Society for Aeronautical and Space Sciences. (pp. 1294-1297). Seoul : KSAS.
  6. H. S. Yeom, J. H. Oh & D. Y. Sung. (2008). Development of the Low Altitude Relay System for Missile Captive flight Test. Daejeon : ADD.
  7. P. S. Kim. (2015). Considerations on the flight test implementation for small airplane certification program. Journal of Aviation Development of Korea, 63, 57-71.
  8. S. K. Kim. (2015). Understanding of structural requirements of airworthiness standard for small airplane. Journal of Aviation Development of Korea, 63, 147-163.
  9. Department of Defense Handbook (1990). Guide to Aircraft/Stores Compatibility (MIL-HDBK-244A). USA : DoD.
  10. M. S. Kim, S. S. Lee & S. J. Kim. (2003). External Store Separation Anaysis and Flight Test Results of XKO-1. Daejeon : ADD.
  11. Department of Defense Interface Standard (2007). Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment (MIL-STD-461F). USA : DoD.
  12. Department of Defense Interface Standard (2010). Electromagnetic Environmental Effects Requirements for Systems (MIL-STD-464C). USA : DoD.
  13. H. S. Yeom, J. H. Oh & D. Y. Sung. (2008). The XKO-1-05 Modification for a Captive Flight Test. Daejeon : ADD.
  14. Department of Defense Handbook (2004). Aircraft/Store Electrical Interconnection System (MIL-HDBK-1760A). USA : DoD.
  15. J. S. Park. (2016). Report of the Preparations and Results for the Installation of the Captive Flight Test POD to the Airplane. Daejeon : ADD.