|
|
论文:2012,Vol:30,Issue(2):279-285 |
|
|
引用本文： |
|
|
聂瑞, 章卫国, 李广文, 刘小雄. 基于时域Neal-Smith准则的人机控制系统设计多目标优化研究[J]. 西北工业大学 |
|
|
Nie Rui, Zhang Weiguo, Li Guangwen, Liu Xiaoxiong. A Fairly Successful Exploration of Multi-Objective Optimization of Aircraft Flight Control System Design Using Time-Domain Neal-Smith Criterion[J]. Northwestern polytechnical university |
|
|
|
|
|
|
|
| 基于时域Neal-Smith准则的人机控制系统设计多目标优化研究 |
|
| 聂瑞, 章卫国, 李广文, 刘小雄 |
|
| 西北工业大学 自动化学院,陕西 西安 710072 |
| 摘要: |
| 为了获得驾驶员和飞机良好的匹配特性,使用基于人机闭环参考模型的方法将飞行品质的要求引入优化算法,进行飞行控制系统设计。首先使用CAP准则建立飞机等效系统模型。然后,基于时域Neal-Smith准则,通过多目标优化算法一次性得到在不同任务条件下的最优驾驶员模型。根据需要选择相应的驾驶员模型,并与飞机等效系统模型组成人机闭环参考模型,进行飞行控制设计多目标优化。仿真结果显示,文中的算法不仅可以整定控制器参数,根据任务需求选取最优驾驶员模型,还可以利用优化结果进行PIO易感性的分析。 |
| 关键词:
飞行控制系统
多目标优化
飞行品质
参考模型
时域Neal-Smith准则
|
|
| A Fairly Successful Exploration of Multi-Objective Optimization of Aircraft Flight Control System Design Using Time-Domain Neal-Smith Criterion |
|
| Nie Rui, Zhang Weiguo, Li Guangwen, Liu Xiaoxiong |
|
| Department of Automatic Control,Northwestern Polytechnical University,Xi'an 710072,China |
| Abstract: |
| Sections 1 and 2 of the full paper explain what we believe to be a fairly successful exploration. Theircore consists of: (1) to match the pilot and the aircraft, with the man-vehicle closed loop reference model, we in-troduce the flight quality requirements into the optimization algorithm to design the aircraft flight control system;(2)we establish the equivalent model of the aircraft with the CAP criterion; (3) using the time-domain Neal-Smithcriterion, we perform the multi-objective optimization to obtain the optimal pilot reference models under differenttasks; (4) we select the optimal pilot reference model according to the flight quality requirements and combine itwith the aircraft equivalent model to form the man-vehicle closed loop reference model; (5) with the man-vehicleclosed loop reference model, we design the aircraft flight control system by using the multi-objective optimization al-gorithm. Section 3 simulates the multi-objective optimization of the pilot reference model and the man-vehicleclosed loop reference model; the simulation results, given in Figs. 5 through 8, and their analysis show preliminari-ly that our multi-objective optimization algorithm can not only tune the parameters of the controller of the aircraftflight control system but also select the optimal pilot reference model under different tasks and use the optimizationresults to evaluate the PIO (pilot-induced oscillation) susceptibility. |
| Key words:
aircraft
algorithms
analysis
closed loop control systems
design
evaluation
man machine sys-tems
models
numerical control
optimization
parameter optimization
requirements engineering
tracking (position)
sensitivity analysis
simulation
standards
time domain analysis;flight controlsystems
multiobjective optimization;flight quality
reference model
time-domain Neal-Smith criteri-on
|
|
| 收稿日期: 2011-05-12
修回日期:
|
| DOI: |
| 基金项目: 航空科学基金(20090753008)资助 |
| 通讯作者:
Email： |
| 作者简介: 聂瑞(1985-),西北工业大学博士研究生,主要从事飞行器控制、智能控制及优化算法的研究。
|
|
|
|
|
|
|
|
参考文献: |
|
|
[1] Anderson M R. Unified Pilot-Induced Oscillation Theory, Volume 3. PIO Analysis Using Multivariable Methods. Virginia Poly-technic Inst and State Univ Blacksburg Dept of Aerospace and Ocean Engineering, 1995
[2] 宁国栋, 方振平. Neal-Smith 时域 PID 预测准则及应用. 北京航空航天大学学报. 2005(4): 407-411Ning Guodong, Fang Zhenping. PID Multi-Objective Optimization Design Based on Pareto Optimality. Journal of Beijing Univer-sity of Aeronautics and Astronautics, 2005(4): 407-411 (in Chinses)
[3] Zhao Z, Liu Y, Yan S W, et al. Pilot-Induced Oscillations (PIO) Susceptibility Evaluation Approach Based on SequentialQuadratic Programming. IEEE, 2010, 468-471
[4] Bailey R E, Bidlack T J. A Quantitative Criterion for Pilot-Induced Oscillations-Time Domain Neal-Smith Criterion, 1996, 598-610
[5] Avanzini G, Minisci E A. Evolutionary Design of a Full-Envelope Flight Control System for an Unstable Fighter Aircraft. IEEE, 2010, 1-8
[6] 刘楠楠, 石 玉, 范胜辉. 基于 Pareto 最优的 PID 多目标优化设计. 信息与控制, 2010(4): 385-390Liu Nannan, Shi Yu, Fan Shenghui. PID Multi-Objective Optimization Design Based on Pareto Optimality. Information andControl, 2010(4): 385-390 (in Chinese)
[7] 李学斌. 基于多目标遗传算法和多属性决策的船舶柴油机转速 PID 控制器参数优化. 海军工程大学学报, 2009, 21(003): 61-65Li Xuebin. Multi-Objective Optimization and Multi-Attribute Decision Making for PID Controller Parameters Tuning in ShipDiesel Design. Journal of Naval University of Engineering, 2009, 21(003): 61-65 (in Chinese)
[8] 高金源, 李陆豫, 冯亚昌. 飞机飞行品质. 北京: 国防工业出版社, 2003Gao Jinyuan, Li Luyu, Feng Yachang. Aircraft Handling Qualities. Beijing: National Denfence Industry Press, 2003 (in Chinese)
[9] Bailey R E, Bidlack T J. Unified Pilot-Induced Oscillation Theory. Volume 4. Time-Domain Neal-Smith Criterion. Calspan Ad-vanced Technology Cenier Buffalo NY, 1995, 8-10
[10] K D, S A, A P. A Fast Elitist Non-Domina2ted Sorting Genetic Algorithm for Multi-Objective Optimization:NSGA2 II. Paris, France: 2000, 1-11
[11] 赵志忠, 刘 艳, 高正红. 基于序列二次规划的 PIO 易感性时域评估方法. 飞行力学. 2010(4): 1-4Zhao Zhizhong, Liu Yan, Gao Zhenghong. PID Susceptibility Evaluation Approach Based on Sequential Quadratic Programming．Flight Dynamics, 2010(4): 1-4 (in Chinese) |
|
|
|
相关文献: |
|
|
1．耿峰, 祝小平, 周洲, 孟俊生.一种有效的高速攻击型无人机二自由度PID控制[J]. 西北工业大学, 2013,31(1): 1-7 |
|
|
|
|
|
|
