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微型扑翼飞行器(FMAV)由于微型化和采用扑翼飞行方式的特征,许多传统理论和设计方法不再完全适用,相关理论和技术仍在不断地发展中,所以对国内外相关理论和技术的发展现状进行及时跟踪和研究,具有非常重要的参考意义;通过调查研究,介绍了与微型扑翼飞行器控制系统有关的低雷诺数非定常空气动力学、控制系统数学模型、控制方案和控制方法等的研究进展,总结出了微型扑翼对飞行器控制系统的设计要求,控制系统的特点和需要解决的关键问题,并展望了未来发展趋势。
Micro flapping wing aircraft (FMAV) Due to the characteristics of miniaturization and the use of flapping-wing flight mode, many traditional theories and design methods are no longer fully applicable, and the related theories and technologies are still being developed. Therefore, relevant theories and technologies at home and abroad The development of the status quo in time to track and study, has very important reference significance; through the investigation and study, introduces the low Reynolds number unsteady aerodynamics, control system mathematical model, control schemes and control methods related to micro flapping-wing aircraft control system The paper summarizes the design requirements of the micro-flapping wing aircraft control system, the characteristics of the control system and the key problems to be solved, and prospects the future development trend.