运输机重装空投模型及控制若干问题综述  

Heavyweight Airdrop of Transport Aircraft: Models and Control Problems

作　　者：刘日 刘永波 徐明 毛瑜昊 姜巍 LIU Ri;LIU Yong-bo;XU Ming;MAO Yu-hao;JIANG Wei(Theory Training Department,Harbin Air Force Flight Academy,Harbin 150000,China;Institute of Aeronautic and Astronautic Engineering,Air Force Engineering University,Xi＇an 710038,China)

机构地区：[1]空军哈尔滨飞行学院理论训练系,哈尔滨150000 [2]空军工程大学航空航天工程学院,西安710038

出　　处：《电光与控制》2018年第11期62-66,72,共6页Electronics Optics & Control

基　　金：国家自然科学基金(61273141);航空科学基金(20141396012)

摘　　要：运输机重装空投是一项前沿和尖端的军事技术,近年来已成为学术界竞相研究的热点。对重装空投过程的动力学模型和飞行控制方法研究现状进行了综述,分析了整体法建模及分离体法建模的优缺点和适用性,研究了线性控制、动态逆控制、滑模变结构控制、反步控制以及模型参考自适应控制等先进控制方法在重装空投控制器设计中的应用情况,讨论了当前重装空投控制器设计中存在的问题与挑战,为下一步的研究提供帮助和借鉴。Heavyweight airdrop of the transport aircraft is an advanced and sophisticated military technology, which has become a research hotspot in the academic field. The research status of the dynamic models and flight control approaches in heavyweight airdrop operations are reviewed in this paper. The advantages, disadvantages as well as the applicability of the integrated modeling method and the separated modeling method are analyzed. The application of such advanced control methods as linear control, dynamic inversion control, sliding mode variable structure control, Backstepping control and model reference adaptive control in the design of heavyweight airdrop controller are studied. The existing problems and challenges in the design of heavyweight airdrop controller are discussed, which is helpful for further research.

关 键 词：重装空投 动力学模型 飞行控制 运输机 

分 类 号：V249[航空宇航科学与技术—飞行器设计]