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ID:33399561
大小:2.71 MB
页数:85页
时间:2019-02-25
《某小型无人倾转旋翼机飞行控制系统设计与仿真》由会员上传分享,免费在线阅读,更多相关内容在行业资料-天天文库。
1、某小型无人倾转旋翼机控制系统设计与仿真ABSTRACTThemaincontentofthisarticlearetwoparts:modelingthenonlinearflightdynamicsoftheaircraftandcontrolsystemdesign.Firstofall,rotoraerodynamicmodelofasmallunmannedtiltrotoraircraftisestablishedbaseonbladeelementTheoryandbycombiningwi
2、thwindtunneltestdataoftheaircraftthewings,fuselage,flattailandverticaltailaerodynamicaremodeled,thencombinetheaerodynamicmodelofeachpartintoacompletenonlinearflightdynamicsmodelofasmallunmannedtiltrotoraircraft.Thenacelleangle-speedflightenvelopeiscalcul
3、atedbytrimmingandanalyzingthenonlinearflightdynamicsmode.linearizethenonlinearmodelbasedonsmallperturbationtheoryandanalysisthestabilityandmaneuverabilityofsmallunmannedtiltrotoraircraft.Designaconversiontrajectoryfromhelicopterflightmodetofixedwingaircr
4、aftflightmode.Secondary,designthecontrollawofsmallunmannedtiltrotoraircraftattitude,accordingtothelinearmodel,usingH∞loopshapingrobustcontrolmethod.Thewholeconversioncorridorisdividedseveralcontrolareas,thenspeedloopcontrollawisdesignedwiththePIDcontrolm
5、ethodonthebasisoftheattitudecontrollaw.Putforwardschedulestrategyofdifferentcontrollers.Completethenonlinearsimulationofattitudecontrol,speedcontrolandconversionprocessaroundthewholeconversioncorridorofsmallunmannedtiltrotoraircraft.Keywords:tiltrotorair
6、craft,flightdynamicsmodel,H∞loopshapingcontrol,conversionsimulation,nonlinearsimulation.II南京航空航天大学硕士学位论文目录第一章绪论...............................................................................................................................11.1研究的意义和目的....
7、........................................................................................................11.2国内外发展概况................................................................................................................11.3飞行力学建模.................
8、...................................................................................................51.4飞行控制...................................................................................................................
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