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飛行器系統概論(第2版) 版權信息
- ISBN：9787118124675
- 條形碼：9787118124675 ; 978-7-118-12467-5
- 裝幀：一般膠版紙
- 冊數：暫無
- 重量：暫無
- 所屬分類：>
飛行器系統概論(第2版) 內容簡介
書介紹了飛行器系統的基本概念和基本原理。主要包括空間環境、力學環境、飛行基本原理、系統組成、推進系統、外形與結構、制導與控制系統、地面設備與發射方式、有效載荷等。還介紹了飛行器設計與研究的基本概念、研究方法和典型實驗等。
本書也可供從事飛行器設計、研究、生產和部隊有關人員參考。
飛行器系統概論(第2版) 目錄
Chapter 1 Brief Introduction to flightvehicles1．1 Basic concepts1．2 Overview of flight vehicles 1．2．1 Rockets 1．2．2 Missiles 1．2．3 Airvehicles 1．2．4 Spacevehicles 1．2．5 Hypersonicflight vehicles1．3 Development history of flight vehicles 1．3．1 Flight vehicle exploration 1．3．2 Typicalexamples of aeronautics & astronautics 1．3．3 Famouspersons in aerospace 1．4 Flight vehicles today 1．4．1 Rockets & missiles 1．4．2 Air vehicles 1．4．3 Space VehiclesChapter 2 Flight principles of flightvehicles2．1 Outlines2．2 Rocket motion 2．2．1Basic principles 2．2．2Multistage rocket theory2．3 Atmospheric environment 2．3．1 Atmosphericenvironment 2．3．2 Standard atmosphere 2．3．3Earth reference ellipsoid2．3 Physical properties of atmosphere 2．3．1 Gas state equation 2．3．2 Low speedflow 2．3．3 High speedflow 2．3．4 Basicprinciples of fluid2．4 Mechanics environment of a flight vehicle 2．4．1Gravity 2．4．2Thrust & thrust moments 2．4．3 Aerodynamics & aerodynamic moments2．5 Flight vehicle motion 2．5．1Reference frames and transformations 2．5．2Flight vehicle motion equation 2．6 Flight performances 2．6．1Flight mission profile 2．6．2Overload2．7 Flight stability & control 2．7．1Stability 2．7．2ControlChapter 3 Flight vehicle system compositions3．1 Overview of flight vehicle system3．2 Missile system composition 3．2．1 Surface toAir missile system 3．2．2 Antitank missile system3．3 Rocket system composition3．4 Aircraft system composition3．5 Spacecraft system composition 3．5．1 Satellitesystem 3．5．2 Spacecraftsystem 3．5．3 Spacestation system 3．5．4 Mannedspace flight systemChapter 4 Flight vehicle propulsion system4．1 Basic concepts and principles4．2 Main performance parameters4．3 Aviation engine system4．4 Rocket propulsion system 4．4．1 Solidrocket propulsion system 4．4．2 Liquidrocket propulsion system4．5 Combination engine system4．6 Thrust vector control system4．7 Special propulsion system4．8 Engine applicationChapter 5 Flight vehicle aerodynamic configuration5．1 Flight vehicle configuration 5．1．1Overview 5．1．2 Typicalmissile configuration 5．1．3 Aircraft configuration 5．1．4 Liftingsurfaces 5．1．5 Controlsurfaces5．2 Flight vehicle configuration parameters 5．2．1 Airfoil 5．2．2Wing platform 5．2．3Flight vehicle configuration geometric parameters5．2 Aircraft configuration variationChapter 6 Flight vehicle construction6．1 Flight vehicle construction6．2．1 Typical construction6．2．2 Body (fuselage) 6．2．3 Wing 6．2．4 Tail6．2 Loads on flight vehicles 6．3．1 Aerodynamicloads 6．3．2 Massdistribution loadsChapter 7 Flight vehicle GNC system7．1 Concepts of GNC system7．1．1 Guidance and control loop7．1．2 Navigation system 7．1．3 Guidance system7．1．4 Control system7．2 Guidance and control components7．2．1 Sensitive components 7．2．2Seeker7．3 Guidance modes 7．3．1 Automaticguidance system 7．3．2 Remoteguidance system 7．3．3 Homingguidance system 7．3．4 Combinationguidance system7．4 Control system 7．4．1 Threecontrol ways 7．4．2 Autopilot7．5 Guidance methods 7．5．1 Automaticguidance method 7．5．2 Remoteguidance method7．6 ActuationChapter 8 Ground equipment and launch8．1 Airport and ground equipment 8．1．1 Airport 8．1．2 Groundequipment8．2 Rocket & space vehicle launch 8．2．1 Space base 8．2．2 Space shuttlelaunch procedure 8．2．3 Spacevehicle return & reentry8．3 Missile launch 8．3．1 Missilelaunch system 8．3．2 Missilelaunch ways 8．3．3 Missilelaunch equipmentChapter 9 Payloads9．1 Outlines9．2 Rocket payloads9．2 Air vehicle payloads9．3 Space vehicle payloads9．4 Missile payloads 9．4．1 Warheadcomposition 9．4．2 Typicalwarhead 9．4．3 FusesChapter 10 Flight vehicle research anddevelopment10．1 Flight vehicle design concepts 10．1．1 Flightvehicle design process 10．1．2 Flightvehicle system analysis10．2 Basic stages of flight vehicle research anddevelopment10．2．1 Idea proposition10．2．2 Proof of tactical and technical requirements10．2．3 Preliminary design10．2．4 Technical design10．2．5 Trial-manufacture and test 10．2．6 Design finality10．2．7 Manufacture and utilization10．3 Design requirement10．4 Design methods10．5 Typical tests10．6 Design example for a flight vehicleReferences
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飛行器系統概論(第2版) 作者簡介
唐勝景，北京理工大學教授、博士生導師。主要從事飛行器設計、飛行力學與控制、新概念飛行器等方面的研究，主持并完成有關飛行器系統論證、概念研究、總體設計、飛行力學與計算機仿真等方面國防科技預研項目十余項，曾獲中國 工業部級科技進步二等獎、三等獎各一項，其中三等獎等。
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