2019
DOI: 10.1016/j.cja.2019.07.001
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A CFD-based numerical virtual flight simulator and its application in control law design of a maneuverable missile model

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Cited by 9 publications
(7 citation statements)
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References 22 publications
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“…More details is given by Zhang et al. 47 The infrastructure and executive is an event-driven infrastructure that is component unaware. The components themselves can produce or respond to events and subscribe to or publish data; thus, the infrastructure and executive are coded once with the use of cases and contributing components specified by the input file.…”
Section: The Integrated Coupling Methods For Fish Self-propelled Swimmmentioning
confidence: 99%
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“…More details is given by Zhang et al. 47 The infrastructure and executive is an event-driven infrastructure that is component unaware. The components themselves can produce or respond to events and subscribe to or publish data; thus, the infrastructure and executive are coded once with the use of cases and contributing components specified by the input file.…”
Section: The Integrated Coupling Methods For Fish Self-propelled Swimmmentioning
confidence: 99%
“…5,6 In addition, the coupled solver without maneuvering control has also been validated with some typical test cases. 36,43,47 So, here we will not repeat them again for brevity.…”
Section: The Integrated Coupling Methods For Fish Self-propelled Swimmmentioning
confidence: 99%
“…Meanwhile, unsteady effects such as the dynamic lift and vortex breakdown also result in challenges to control the aircraft securely. Traditional control law design methods based on linear assumptions with small perturbations are no longer suitable [4]. Hence, aircraft designers call for more accurate methods that consider unsteady effects.…”
mentioning
confidence: 99%
“…In previous work [4,20], the authors also developed an NVF simulation tool, named Hybrid Platform for Engineering and Research of FLOWs-Numerical Virtual Flight Simulator (Hyper-FLOW-NVFS). The NVF simulator integrates an unsteady Reynolds-averaged Navier-Stokes (RANS) solver on dynamic grids, a hybrid dynamic grid generator, a rigid-body dynamics solver, and a user-defined flight control system (FCS).…”
mentioning
confidence: 99%
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