Fig. 1 Overview of FHME
Fig. 2 Main menu of FHME
Fig. 3 “Air-Vehicle in flight” menu of FHME
Fig. 4 Operation procedure of FHME
Fig. 5 Verification test procedure of FHME
Fig. 6 System Integration Laboratory(SIL) test process of FHME
Fig. 7 Description for on-board equipment interface test of FHME(TC-004)
Table 1 Software requirements of FHME
Table 2 Environment requirements of FHME
Table 3 FHME acceptance test items
Table 4 Acceptance test results of FHME
Table 5 System Integration Laboratory(SIL) test results
Table 6 Items of on-board equipment interface testing
References
- J. W. Lim, "A Study on the Safety of Flight(SOF) Assure through Aircraft Diagnostics Systems", Journal of Aerospace System Engineering, vol. 11, no 1, pp. 35-40, 2017 https://doi.org/10.20910/JASE.2017.11.1.35
- S. E. Shin, "BIT Design Objective and Verification Method in UAV System Development", Avionics Systems Symposium Korea 2015, vol. 2015, pp. 347-354, July. 2015
- J. S. Kim, S. Y. Yang, J. P. Han, "The BIT Design for Identifying Malfunction in Avionics", 2014 KSAS fall Conference, November. 2014
- D. W. Yoo, S. M. Cho, H. S. Ha, K. M. Cho, "System Integration Test Environment Setup and Testing Method for Interface Verification of Unmanned Aerial Systems", 2018 KIMST Conference, pp. 2155-2156, June. 2018
- S. M. Cho, D. W. Yoo, J. I. Shim, H. S. Ha, "Environment Design and Verification Test Method of System Integration Lab for UAS", 2018 KIMST Conference, pp. 2153-2154, June. 2018