Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS》 1994-03
Add to Favorite Get Latest Update

A HYBRID SIMULATION STUDY OF NONLINEAR DECOUPLING CONTROL SYSTEM FOR AIRCRAFT PENETRATION

Chen Yanyang;Sun.Baoting; Hu Zhaofeng(Beijing University of Aeronautics and Astronautics. Dept. of Flight Vehicle Design and Applied Mechanics)  
While an aircraft penetrates at low level by using TF/TA technologies.there appears tohave some nonlinear cross couple between longtudinal and lateral movement.A flight controllaw by combining the nonlinear inverse dynamics theory and the modern optimal control theory can be founded to decouple the coupling motion. This paper mainly deals with the hybridsimulation of this nonlinear decoupling control system. A mathematical model for simulationand the simulation mathod are provided. Some researching results in system's decouplingcontrol of the aircraft flying in atmosphere with and without turbulent disturbance: insystem's capturing the command input and in aircraft flying qualities are presented. The simulation results illustrate that the system can accurately capture the desired three demensionalpenetration trajectary by decoupling control laws and it offers better dynamic characteristicsand flying qualities of the aircraft even encountering the atmosphere disturbance.
【Fund】: 航空科学基金
【CateGory Index】: V249.122
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
【References】
Chinese Journal Full-text Database 2 Hits
1 WU Hu-zi;WANG Jin;L Xin-bo;HUANG Zhen-wei;AVIC,The Center of Research and Development;;Analysis of Safety Constraints with Low Altitude Penetration in Serious Atmosphere[J];现代防御技术;2017-04
2 Sun Baoting, Chen Yanyang (Faculty 509 of Beijing University of Aeronautics and Astronautics, Beijing, 100083);PILOT-VEHICLE SEMI-PHYSICAL SIMULATION STUDY OF DECOUPLING CONTROL FOR AIRCRAFT TF/TA PENETRATION[J];航空学报;1995-03
【Citations】
Chinese Journal Full-text Database 1 Hits
1 Sun Baoting Chen Yanyang (Beijing University Aeronautics and Astronautics);Real-Time Simulation Implementation of Nonlinear Decoupling Control for Aircraft Penetration Flight[J];系统仿真学报;1994-04
【Co-citations】
Chinese Journal Full-text Database 3 Hits
1 Sun Baoting ; Jiang Zhiqiang(Beijing University of Aeronautics and Astronautics);REAL TIME SIMULATION TECHNIQUE STUDY OF INTEGRATION FOR FLIGHT DYNAMICS SYSTEM[J];飞行力学;1995-02
2 Sun Baoting, Chen Yanyang (Faculty 509 of Beijing University of Aeronautics and Astronautics, Beijing, 100083);PILOT-VEHICLE SEMI-PHYSICAL SIMULATION STUDY OF DECOUPLING CONTROL FOR AIRCRAFT TF/TA PENETRATION[J];航空学报;1995-03
3 Chen Yanyang;Sun.Baoting; Hu Zhaofeng(Beijing University of Aeronautics and Astronautics. Dept. of Flight Vehicle Design and Applied Mechanics);A HYBRID SIMULATION STUDY OF NONLINEAR DECOUPLING CONTROL SYSTEM FOR AIRCRAFT PENETRATION[J];北京航空航天大学学报;1994-03
【Co-references】
Chinese Journal Full-text Database 6 Hits
1 JIANG Ling-ling,CHEN Huai-min,JIA Bao-juan(National Key Laboratory of UAV Special Technology,Northwestern Polytechnical University,Xi'an Shanxi 710065,China);Study on Low Altitude Penetration Path Planning Algorithm under Flexibility Restraints[J];计算机仿真;2011-08
2 PU Hong-bin1,2,ZHAN Hao1(1.College of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China;2.The General Configuration and Aerodynamic Design and Research Department,The First Aircraft Institute,Xi'an 710089,China);Research on the Trajectory Optimization of Low Altitude Penetration[J];飞行力学;2008-03
3 MA Yun-hong,ZHOU De-yun (Northwestern Polytechnical University,Xi'an 710072,China);Research on Route Planning Algorithm and Constructing Threat Modeling for Aircraft in Low Altitude Penetration[J];火力与指挥控制;2004-05
4 Sun Baoting Chen Yanyang (Beijing University Aeronautics and Astronautics);Real-Time Simulation Implementation of Nonlinear Decoupling Control for Aircraft Penetration Flight[J];系统仿真学报;1994-04
5 Chen Yanyang;Sun.Baoting; Hu Zhaofeng(Beijing University of Aeronautics and Astronautics. Dept. of Flight Vehicle Design and Applied Mechanics);A HYBRID SIMULATION STUDY OF NONLINEAR DECOUPLING CONTROL SYSTEM FOR AIRCRAFT PENETRATION[J];北京航空航天大学学报;1994-03
6 Zheng Yangao(Nanjing Aeronautical Institute);TERRAIN FOLLOWJNG AVOIDANCE TECHNIQUE OF VERY LOW ALTITUDE PENETRATION[J];航空学报;1985-04
【Secondary References】
Chinese Journal Full-text Database 1 Hits
1 Jiang Zhiqiung, Sun Baoting (Beijing University of Aeronautics and Astronautics);Research and Development of Integrated Simulation Software package for NLFDS[J];计算机仿真;1996-03
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved