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A Review of Wind Tunnel Based Virtual Flight Testing Techniques for Evaluation of Flight Control Systems
2015
International Journal of Aerospace Engineering
Wind tunnel based Virtual Flight Testing (VFT) is a dynamic wind tunnel test for evaluating flight control systems (FCS) proposed in recent decades. It integrates aerodynamics, flight dynamics, and FCS as a whole and is a more realistic and reliable method for FCS evaluation than traditional ground evaluation methods, such as Hardware-in-the-Loop Simulation (HILS). With FCS evaluated by VFT before flight test, the risk of flight test will be further reduced. In this paper, the background,
doi:10.1155/2015/672423
fatcat:nfdnoks3qjcntgikqg6tmsql3y