摘要
在气动伺服弹性技术综合方面开展了如下的研究：气动伺服弹性的建模；控制律的综合设计；自适应控制的可行性；主动控制系统的鲁棒稳定性；以及控制律的工程评估等综合问题．这些问题的讨论，都在同一算例上实施的，实验或计算的结果。
Some investigations on aeroservoelasticity synthesis were developed.It involves a series of problems,such as the modelling of aeroservoelasticity,design of control law,feasibility of a adaptive control,robustness stability of active control system and evaluation for engineering properties of control law.These investigations were implemented by using the same flutter model of wing/store,therefore,all the synthesized results can be contrasted no matter what kind of results are,test or calculation.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1996年第3期279-283,共5页
Journal of Beijing University of Aeronautics and Astronautics
基金
航空科学基金
