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김태연(Tai Y. Kim),양태수(Tae S. Yang),김영주(Young J. Kim),이종하(Jong H. Ree) 대한전자공학회 1992 대한전자공학회 학술대회 Vol.1992 No.10
In this paper, the Hardware-In-The-Loop Simulation (HILS) of missile systems are studied. The HILS is an effective performance evaluation technique that bridges the simulation fidelity gap between analytic all-digital simulations and actual flight tests of missile systems. The HILS may be required to perform system integration tests, performance evaluation at system or subsystem level. Major elements of this HILS facility will include the flight table, simulation computers, I/O computer and peripheral equipments. HILS of missile systems typically involve computer modeling of flight dynamics coupled with a hardware guidance and control(G/C) systems. This paper describes a real time performance evaluation technique of a G/e system. Development of a HILS for a Autopilot of SAM G/C will be used as an example.