ESB_Deep_Dive_v8
Linux设备驱动程序(中文版第三版)
Linux 设备驱动 Edition 3ByJonathan Corbet,Alessandro Rubini,Greg Kroah-Hartman由 quickwhale 翻译的简体中文版 V0.1.0 2006-6-2学习编程有几年了，感觉走了不少弯路，而不少的学弟学妹又在重蹈我当初的覆辙，不免有些痛心。
最近在网上也看了许多前辈们的经验建议，再结合自己的学习经历在这里谈谈基础的重要性，希望帮助大家少走些弯路。
什么是基础呢？就是要把我们大学所学的离散数学,算法与数据结构，操作系统，计算机体系结构，编译原理等课程学好,对计算机的体系,CPU本身,操作系统内核,系统平台,面向对象编程,程序的性能等要有深层次的掌握。
初学者可能体会不到这些基础的重要性，学习jsp,donet,mfc,vb的朋友甚至会对这些嗤之以鼻,但是一开始没学好基础就去学jsp或donet会产生很坏的影响,而且陷入其中不能自拔。
我上大二的时候还对编程没什么概念,就上了门C++也不知道能干什么，老师说MFC也不知道是什么东西，看别的同学在学就跟着学了,然后就了解到.net,j2ee,php是什么了，就觉得软件开发就是用这些了，而上的那些专业课又与我们学的sqlserver啊,css啊,ajax啊,毫无关系,就感慨啊，还不如回家自学去就为一个文凭吗？还不如去培训,浪费这么多钱.于是天天基本上没去上什么课,天天就在做网站,几个学期就做了三个网站。
感觉做这些网站就是学到些技巧，没什么进步,这些技巧就好比别人的名字,告诉你你就知道了,网上也都可以搜到。
那时候就觉得把.net学好就行了，搞j2ee的比较难，搞api编程就别想了，操作系统更是望尘莫及了。
后来随着学习的深入和看了网上许多前辈们的建议才对这些基础的重要性有所体会。
虽然.net或java的开发并不直接用到汇编,操作系统这些,但是不掌握这些基础是有很大问题的，因为你只知其然不知其所有然，在mfc和.net里面控件一拖什么都做好了，很方便，但是出了问题可能就解决不了，有些在网上搜都搜不到。
Autodesk Nastran 2022 用户手册说明书
MPA, MPI (design/logo), MPX (design/logo), MPX, Mudbox, Navisworks, ObjectARX, ObjectDBX, Opticore, Pixlr, Pixlr-o-matic, Productstream,
Publisher 360, RasterDWG, RealDWG, ReCap, ReCap 360, Remote, Revit LT, Revit, RiverCAD, Robot, Scaleform, Showcase, Showcase 360,
TrueConvert, DWG TrueView, DWGX, DXF, Ecotect, Ember, ESTmep, Evolver, FABmep, Face Robot, FBX, Fempro, Fire, Flame, Flare, Flint,
ForceEffect, FormIt, Freewheel, Fusion 360, Glue, Green Building Studio, Heidi, Homestyler, HumanIK, i-drop, ImageModeler, Incinerator, Inferno,
Autodesk Nastran 2022
Reference Manual
Nastran Solver Reference Manual
v8引擎使用方法
v8引擎使用方法摘要：1.V8引擎简介2.V8引擎的安装与配置3.V8引擎的使用方法4.V8引擎的优化与调试5.总结与建议正文：v8引擎是一款高性能的javascript引擎，由Google开发，广泛应用于Chrome浏览器和Node.js环境中。
本文将详细介绍v8引擎的使用方法，帮助你更好地掌握这款强大的引擎。
一、V8引擎简介V8引擎是一款开源的、基于单线程的javascript引擎。
它采用了创新的异步执行技术，能够在单个线程中并行执行多个javascript任务，提高了程序的运行效率。
此外，V8引擎还具有内存管理高效、垃圾回收快速等特点，使得它在处理大型javascript应用程序时表现出色。
二、V8引擎的安装与配置1.安装：在Chrome浏览器中，v8引擎已经默认启用。
你可以在设置中检查当前使用的引擎版本。
2.配置：在Node.js环境中，可以通过npm安装v8引擎的版本控制工具，如nvm或n，方便在不同项目之间切换引擎版本。
三、V8引擎的使用方法1.基本语法：与传统javascript引擎相比，v8引擎的语法并无太大差异。
你可以按照现有javascript知识进行编程。
2.异步编程：v8引擎擅长处理异步任务，可以使用Promise、async/await等语法进行异步编程。
3.Web Workers：在Chrome浏览器中，可以使用Web Workers技术在后台线程中运行javascript代码，减轻主线程的负担。
四、V8引擎的优化与调试1.性能优化：针对v8引擎的特点，可以采用如事件驱动、模块化、代码分割等优化策略。
2.调试：使用Chrome浏览器的开发者工具或Node.js的调试工具进行代码调试。
五、总结与建议V8引擎凭借其高性能和优秀的内存管理，成为了现代前端开发的基石。
掌握v8引擎的使用方法，可以提高你的编程效率，使你的项目在性能上更上一层楼。
在日常开发中，要注意合理利用v8引擎的特点，如异步编程、性能优化等，以充分发挥其潜力。
deep security 8.0常见问题处理方法
目录一. 安装部署 (4)Deep Security 8.0是否支持使用IDE 磁盘控制器的VM 虚拟机？ (4)Deep Security 部署在虚拟化环境时需要作哪些准备？ (4)Deep Security 8.0 在企业vSphere 5.0 环境部署时无代理保护时有哪些注意事项？ (5)Deep Security Manager的软硬件需求是什么？ (6)DSVA保护超过25台VM时，DSVA的内存推荐值，ESX的Heap Memory增加值和计算方法 (7)如何vShield Endpoint 5.0 驱动程序？ (8)如何为ESXi5.0使用Update Manager安装vShield Manager补丁 (8)Deep Security 8.0 SP1 支持从哪些版本升级？ (10)Deep Security 8.0 SP1 是否支持ESX/ESXi4.1 和ESXi5.0 混合虚拟化环境？ (11)如何批量升级虚拟机Vm Tools，并加载vSheld Endpoint Thin Driver 驱动 (11)二. 策略设置 (13)Deep Security Anti-malware对于Domino服务器的推荐例外设置是什么？ (13)如何针对自动创建的虚拟机和移动的虚拟机进行自动激活和分配策略? (14)如何取消DSA 8.0 客户端自我保护功能 (16)当DS8.0工作在内外网隔离环境时如何更新DS 产品组件？ (17)Deep Security 8.0 帐号被锁定时如何进行解锁 (17)当忘记Deep Security Manager 登录密码时如何重置管理控制台密码？ (18)三. 常见故障处理 (18)为什么会出现Smart Scan 中断问题 (18)Deep Security 启用DPI Event 日志中出现大量＂URI 中的字符非法＂日志记录 (18)Deep Security 8.0 执行"准备"ESXi服务器时提示“操作不成功----There was an error resolving dependencies.” (19)Deep Security 8.0 遇到更新问题时需要收集哪些信息？ (19)Deep Security Manager(DSM)8.0 安装时提示“JVM could not be started”安装无法继续？........................................................................... (19)Deep Security Agent执行恶意软件手动扫描时提示报错“于客户端/设备发生以下错误，无法完成此操作: -1”应如何处理？ (19)四. 其他 (20)Deep Security Relay 的作用是什么？............................................20Deep Security 8.0 FAQ3Deep Security 7.5的激活号是否可以用来激活Deep Security 8.0 (20)Deep Security Agent 是否可以通过DSM 管理控制台卸载？ (20)当DSA 无法与DSM 通讯时是否支持离线更新？ (20)Deep Security 8.0 SP1 中新增功能无代理完整性监控是否支持实时监控? (20)一. 安装部署Deep Security 8.0是否支持使用IDE 磁盘控制器的VM 虚拟机？由于vShieldEndpoint 5.0 不再限制支持范围为SCSI LSI logic控制器，因此DS 8.0 虚拟机即时采用IDE 磁盘格式也支持Agent-less Anti-malware功能。
SpagoBI开源BI平台_安装配置及使用说明v15
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SpagoBI-开源 BI 平台软件安装配置与使用说明
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肖渺 ****-**-** 公开 1.5
【 SpagoBI 开源 BI 平台软件 】 【安装配置与使用说明】
2012 年 09 月
SpagoBI-开源 BI 平台软件安装配置与使用说明
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黑翼飞行模拟器用户手册说明书
IntroductionThe Blackwing BW 635RG is an ultralight two-seater aeroplane designed for recreational flying and training purposes. It features a sleek and modern design, with a composite airframe and a low-wing configuration. The Blackwing has a cruising speed of up to 120 knots and a range of approximately 700 nautical miles, making it suitable for both short and long-distance flights. The cockpit is equipped with state-of-the-art avionics, including a glass cockpit display and an autopilot system. The Blackwing is also known for its superior handling and stability, making it a popular choice among flying enthusiasts and flight schools. The BW 635RG is powered by the venerable Rotax 915 iS engine.Development Credits:Mal Cartwright Product LeadRuss White3D Modelling, Interior and Exterior TexturingJack Lavigne IntegrationHarry Stringer AnimationPropAir Flight Model and SystemsJordan Gough ManualWith special thanks to our Beta Testers:Rob Abernathy John BurgessNick Cooper John DowMatt McGee Darryl WightmanTable of ContentsIntroduction (2)Development Credits: (2)With special thanks to our Beta Testers: (2)Table of Contents (3)Notes on Hardware (4)Overview (5)Aircraft Limitations (6)Airspeed Limitations (6)Engine Limitations (6)Operating Conditions (6)Fuel (7)Other Limitations (7)Emergency Procedures (8)Engine Failure on the Take-off Roll (8)Engine Failure after Take-off (8)Glide Performance (8)Emergency Landing (9)Spin Recovery (9)Normal Procedures (10)Before Starting Engine (10)Starting Engine (10)Before Taxiing (11)Taxiing (11)Engine Runup (11)Before Take-off (11)Take-Off (12)Initial Climb (12)Cruise Climb (12)Cruise (12)Landing (13)Balked Landing (13)After Landing (13)Securing Aircraft (14)Basic Performance (15)Stall Speeds (15)Take-Off Performance (15)Landing Performance (16)Systems Description (17)Instrument Panel Layout (17)Switch Logic and Electrical System (18)Master Switch (18)Fuel Pump Switch (19)LAND/TAXI Switch (19)Strobe/Nav Switch (19)Electrical System Diagram (20)Engine (21)Propeller (21)Fuel (21)Notes on HardwareDue to the unusual 3-position switches in this aircraft, conventional hardware 2position toggle switches (eg. strobe or nav light switches) cannot be translated tothe single 3-position switch which combine these.Additionally, as this aircraft utilises a single level power control (throttle), conventional throttle/prop/mixture hardware may interfere with the function of this system, and not work as intended. It is recommended to place your propeller and mixture levers in the IDLE position, and not move them while the engine is running.OverviewThe Orbx BW 635RG has been developed using official documentation and Computer Aided Design (CAD) resources from Blackwing Sweden. As a result, the aeroplane has been created through masterful modelling, texturing, systems integration, and flight model development.Figure 1 – Aircraft 3-viewAircraft DimensionsLength 6.6m Height 2.2m Wingspan8.4mWeightsBasic Empty Weight 375kg Maximum Take-off Weight 600kg Maximum Fuel Capacity (Litres)130LThe content in this manual and the operation of the BW 635RG in Microsoft Flight Simulator strictly must not be used as reference material in any form for operating the real aircraft.Aircraft LimitationsAirspeed LimitationsAirspeed Description Airspeed (KIAS) RemarksVne Never Exceed Speed 157 Must not exceed this speed in any operation.Va Manoeuvring Speed 109 If full or abrupt control deflection is made, the airframe may be overstressed.Vfe1 Max flap extended speed20 degrees90 Maximum speed for flaps 20°Vfe2 Max flap extended speed35-45 degrees 70 Maximum speed for flaps 35-45°Vlo Maximum landing gearoperating speed 70Do not extended or retract the landing gearabove this speed.Vle Maximum landing gear extended speed 90 Do not exceed this speed with the landing gearalready down.Vs0 Stall speed flaps/gearextended 38 Stall speed with gear down/flaps >0° and in level flight at MTOWVs1 Stall speed clean 49 Stall speed flaps retracted, gear up and in level flight at MTOWEngine LimitationsEngineEngine Manufacturer Rotax Engine Model Rotax 915 iSMaximum Power Take-off (Max 5 min.) 141 hp Continuous 135 hpMaximum RPM Take-off (Max 5 min.) 5800 Continuous 5500Critical Altitude 15000ft AMSL Maximum OperatingAltitude23000ft AMSL Operating ConditionsAerobatic manoeuvres, flight in IFR conditionsand flights in icing conditions are prohibited inthis aircraft.FuelFuel TanksLeft Right Litres US Gal Litres US GalTotal Fuel in Tank 67.5 17.8 62.5 16.5Unusable Fuel 2.5 0.7 2.5 0.7 Total Useable Fuel in Tanks 66.5 17.6 61.5 16.2Other LimitationsMaximum demonstrated crosswind for the BW 635RG is 20 knots.Emergency ProceduresNote: The following procedures have been modified to be suitable for simulation. It does not cover emergencies that are a) not simulated and b) not reasonable. Checklist items from the real procedures have been omitted and these procedures must not under any circumstances be used for training purposes.Engine Failure on the Take-off RollThrottle: IDLEIgnition: OFFFuel Pump: MAIN (DOWN POS)Brakes: APPLYWhen stopped: SECURE AIRCRAFTEngine Failure after Take-offNose: IMMEDIATELY LOWERAirspeed: 65 KNOTSLanding Area: DETERMINE WITHIN 30° OF NOSEFlaps: USE AS REQUIREDLanding Gear: USE DESCRETIONFuel Selector: OFFIgnition: OFFMaster Switch: OFFGlide PerformanceThe BW 635RG, the approximate performance for a glide is 65 KIAS which willgive approximately a 545ft/min rate of descent in the clean configuration.Glide performance will degrade significantly on extension of flaps and landinggear.Emergency LandingAirspeed: 65 KIASField: PICK BEST OPTIONLanding Gear: USE DISCRETION DEPENDING ON FIELD TYPEFlaps: AS REQUIREDFuel Selector: OFFIgnition: OFFFuel Pump: MAIN (down)Master Switch: OFF BEFORE LANDINGSpin RecoveryThrottle: IDLEControl Stick: AILERON NEUTRALRudder: FULL OPPOSITE TO DIRECTION OF ROTATIONControl Stick: POSITIVELY FORWARD OF NEUTRALRudder: NEUTRAL WHEN ROTATION STOPSControl Stick: SMOOTHLY PULL OUT OF DIVEWARNING:INTENTIONAL SPINS ARE NOT APPROVED INTHIS AIRCRAFT.Normal ProceduresNote: The pre-flight inspection portion of the normal procedures has been removed due to impracticality in the simulator.Before Starting EngineIgnition: OFFMaster Switch: OFF (down)Backup Battery: OFF/AUTO (down)Landing Gear Lever: DOWNCircuit Breakers: INCanopy CLOSED (CLICKING THE LATCHON THE INSIDE LEFT SIDEWALL.) Starting EngineParking Brake: HOLD TOE BRAKES AND ENGAGE PARKINGBRAKEMaster Switch: ENGINE START (middle position)Fuel Selector: SETFuel Gauge: CHECKFuel Pump: BOTH (up)Ignition: BOTHNav Lights: STROBE (middle position)Throttle: SET ½-1 INCH OPENIgnition: STARTOil Pressure: GREEN WITHIN 10 SECWarnings: NONEBefore TaxiingMaster Switch: NORMAL OPERATION (up)Altimeter: SETAvionics: SETParking Brake: DISENGAGETaxiingInstruments: CHECKED (COMPASS/HSI/BALL/ATT) Engine RunupParking Brake: ENGAGERPM: 2500 RPMFuel Pump: CYCLE, CHECK FUEL PRESSUREIdle: CHECK IDLE 1800 +/- 100 RPM Before Take-offCanopy: CLOSED AND LOCKEDFlaps: 1 STAGE (20°)Elevator Trim: SET FOR TAKE-OFFEngine Instruments: NORMALLanding Light: ON (up)Controls: FULL FREE AND CORRECT MOVEMENTParking Brake: DISENGAGETake-OffThrottle: FULLControls: NEUTRAL45 Knots: ROTATEAccelerate: NOSE ON HORIZON, ACCEL TO 80 KIASPositive Rate of Climb: GEAR UPLanding Light: OFF (down)Flaps: RETRACT ABOVE 500’ AGLInitial ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 90 KIASFuel Pump: MAIN (down) ABOVE 500’ AGL Cruise ClimbThrottle: MAX CONTINUOUS (5500 RPM)Airspeed: 130 KIASCruiseThrottle: 55-75% PowerAirspeed: 120-157 KIAS (<130 KIAS IN TURB)LandingFuel: QTY CHECKEDFuel Selector: FULLEST TANKFuel Pump: BOTH (up position)Airspeed: 90 KIASFlaps: EXTEND FLAP 1 <90 KIASDownwind Airspeed: 65 KIASLanding Gear: DOWN @ 65 KIAS; CHECK 3 GREENLanding Light: ON (up position)Base Leg: EXTEND FLAP 2 < 65 KIASFinal Approach Airspeed: 60 KIASBalked LandingThrottle: SMOOTHLY INCREASEAirspeed: 60 KIASTrim: COURSE TRIM TO RELIEVE PRESSUREFlaps: RETRACT TO POSITION 1 (20°)Gear: UPTrim: TRIM FOR CLIMBAfter LandingFlaps: RETRACTExterior Lights: AS REQ’DFuel Pump: MAIN (down)Securing AircraftParking Brake: ENGAGEDThrottle: IDLESwitches: ALL OFF EXCEPT ACL AND MASTERIgnition: OFFNav Lights: OFF (down)Master Switch: OFFBasic PerformanceStall SpeedsMTOW 600kg | CG 32% MAC | Power Idle | Level FlightFlap Position Stall Speed (KIAS) 0° 49 20° 44 35° 39 45°38Take-Off PerformanceMTOW | ISA CONDITIONS | SEA LEVEL | FLAPS 1 (20°) | MTOW (600kg)Cruise PerformanceRunway Surface Ground RollOver 50ft Obstacleft mft mPaved Runway328 100 656 200 Unpaved (Grass) Runway 361110689208Pressure Altitude Power (%) TAS Fuel Flow LPH MAP (inHg) Endurance(hr)Range (nm) 500055 161 19.7 30 5.8 941 65 170 23.3 34.1 4.9 827 7517826.937.44.1738Landing PerformanceMTOW | ISA CONDITIONS | FLAPS 2 (35°) | MTOW (600kg) | Speed 1.3 x VsoRunway Surface Ground Roll Over 50ft Obstacle ft m ft mPaved Runway 525 160 951 290 Unpaved (Grass) Runway 558 170 984 300Systems Description Instrument Panel LayoutSwitch Logic and Electrical SystemThe electrical switches in the BW 635RG are 3-position switches. These are generally known as “DOWN”, “MIDDLE” and “UP”. They are briefly explained below.Master SwitchThe MASTER switch functions in a unique way, with the following switch logic:1.When the MASTER switch is DOWN, all battery power is off. There will beno electrical power provided to the aircraft.•Note: The engine CANNOT be shut down when the master switch isoff. Electrical power must be present for the engine to turn off.2.When the MASTER switch is in the MIDDLE (Engine Start) position, limitedsystem functionality will be present. The backup battery will be activatedand power the following systems:•Primary Flight Display•Compass•AHRS (Attitude Heading Reference System)•Radio3.When the MASTER switch is UP (Normal Operation), full electrical supplywill be provided to the aircraft. The following systems will be powered on: •Note: the engine CANNOT be started with the MASTER switch in theUP position. If the engine won’t start, check the switch is in theMIDDLE position•Multi-Function Display•Transponder•Autopilot•Audio panel•STBY instruments•Pitot Heat•Main battery is disconnected from running engine. Alternatorprovides power.See Section NORMAL PROCEDURES for positioning of the MASTER switch.Fuel Pump SwitchThe Fuel Pump switch also has some advanced logic to it, due to two fuel pumpsbeing present, however, to put it simply, it operates in the following way:1.In the DOWN position, the main fuel pump is in use.2.In the MIDDLE position, the auxiliary fuel pump is in use.3.In the UP position, both fuel pumps will be on.LAND/TAXI SwitchThe LAND/TAXI switch powers the Taxi and Landing lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the taxi light will switch on when the landinggear is extended.3.In the UP position, the Landing Light will switch on when the landinggear is extended.Strobe/Nav SwitchThe Strobe/Nav switch powers the Navigation (Red/Green) and Strobe (flashingwhite) lights. It operates in the following logic:1.In the DOWN position, both lights will be OFF.2.In the MIDDLE position, the STROBE light will be on.3.In the UP position, both the strobe and Nav lights will be on.Electrical System DiagramThe BW 635RG’s electrical system is modelled in the following way in Microsoft Flight Simulator.Because the starter system is connected to the BACKUP BUS, this means you cannot start the engine with the MASTER switch in the UP position, due to the BACKUP BUS being disconnected from the circuit once the MAIN BAT BUS is powered.Page 21 of 21User Guide v1.0 –RevisionEngineThe BW 635RG is powered by the Rotax 915iS. The Rotax 915iS is a four-stroke, four-cylinder, fuel-injected, turbocharged aircraft engine with a maximum power output of141 horsepower. The engine utilizes electronic fuel injection (EFI) technology toprovide precise fuel delivery and improved fuel efficiency. It also features a modernliquid-cooling system and a dual electronic ignition system for reliable performance.The Rotax 915iS engine has a maximum operating RPM of 5,200, with a recommended continuous operation range of 5,000 RPM or less.PropellerThe propeller is a 3-blade wood-composite design, which is hydraulically adjustable for operation at various pitch angles, controlled independently of the pilot. The propeller is linked to the engine through an electronically controlled governor, where RPM isadjusted in accordance with the position of the throttle control. This pitch curve cannot be adjusted in flight, however is designed to ensure maximum performance in allphases of flight.FuelBoth wings have fuel tanks, which are fed to the engine via electric fuel pumps. Fuelsystem information is fed via sensors to the Garmin avionics suite and can be viewedon the displays inside the cockpit.AIRPLANE WEIGHTSBasic Empty Weight……………………….…375 KgMaximum Takeoff Weight…………………..600 KgMaximum Fuel Weight………………………...95 Kg Maximum Landing Weight………………….600 Kg TANK USABLE FUEL LEFT WING TANK67.5 litres 17.8 US Gallons RIGHT WING TANK62.5 litres 16.5 US Gallons TOTAL 130 litres34.3 US GallonsFUEL CAPACITY AIRSPEEDS Never Exceed Speed ……….…………….173 KIAS Max Structural Cruising Speed…………..156 KIAS Maneuvering Speed MTOW……………….109 KIAS Initial Climb………………………………………80 KIASBest Angle Climb……………………………….75 KIASBest Rate of Climb……………………………..90 KIASMax Flap Ext 20°……………………..............90 KIASMax Flap Ext 35-45°……………………………70 KIASMax Landing Gear Operation……………….70 KIASMax Landing Gear Extended………………..90 KIASPlanned Cruise TAS………………………….130 KIASFinal Approach Speed………………………..60 KIAS POWERPLANT LIMITATIONSENGINE LIMITS (RPM)Take-off (5 Minutes)………....5800 RPM Max Continuous……………….5500 RPMALTITUDE LIMITSMaximum Operating Altitude………………23 000ftFor Microsoft Flight Simulator Use Only0-12023 Orbx Simulation Systems Pty. Ltd BW 635RG QUICK REFERENCESHEETIssued: 21 Apr 2023Revised: 21 Apr 20230-2PROCEDURESBEFORE STARTING ENGINEPreflight Inspection………………………….COMPLETECrew Briefing………………………………….COMPLETEIgnition…………………………………………………….OFFMaster Switch…………………………………………..OFFBackup Battery …..…………………………….OFF/AUTOLanding Gear Lever………………………………..DOWNCircuit Breakers…………………………………………..IN Canopy………………………………………………CLOSED STARTING ENGINEArea……………………………………………………..CLEARParking Brake……………….HOLD TOE BRAKES ANDENGAGEMaster Switch …..……………….ENGINE START (MID)Fuel Selector…………………………………………….SETFuel Pump………………………………………BOTH (UP)Ignition………………………………………………….BOTHExternal Lights……………………………………..AS REQThrottle ………………………..………..Τ12-1 INCH OPENIgnition………………………………………………….START AFTER START Oil Pressure.…………………………………………RISING Master Switch ……………………………..NORMAL (UP)Radios………………………………………………………SET Altimeter…………………………………………………..SET ATIS and Clearance…………………………..OBTAINEDBEFORE TAXIBrakes/Park Brake ………………………….DISENGAGEFlight Instruments……………………………..CHECKEDCompass…………………………………………CHECKED BEFORE TAKEOFFCanopy/Harnesses………………………………SECURE Flaps…………………………………….……1 STAGE (20°)Trim ..……………………………………SET FOR TAKEOFF Flight Instruments………………………………………SET Engine Instruments………………CHECKED NORMAL Avionics…………………………………………………….SET External Lights………………………………………AS REQ Flight Controls…………..FULL, FREE AND CORRECT Takeoff Safety Brief………………………….DELIVERED TAKEOFFBrakes/Park Brake………………………….DISENGAGEPower…………SMOOTHLY INCREASE TO MAXIMUM45 knots………………………………………………ROTATEAccelerate……….…NOSE ON HORIZON, TO 80 KTSPositive Rate of Climb………………………….GEAR UPLanding Light.……………………………….OFF (DOWN)Flaps ………………………..RETRACT ABOVE 500’ AGLMEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd ENGINE RUN UP Parking Brake ……………………………………..ENGAGE Engine Instruments……………………………CHECKED Engine RPM…………………………………SET 2500 RPM Fuel Pump…………………………………………….CYCLE Idle …………………..…..CHECK IDLE 1800 ±100RPM Navigation Equipment …..…………………………….SETFor Microsoft Flight Simulator Use OnlyIssued: 21 Apr 2023Revised: 21 Apr 2023AFTER TAKEOFF Engine Instruments……………………..WITHIN LIMITS Climb Speed…………………………………………90 KIAS Fuel Pump………….MAIN (DOWN ) ABOVE 500’ AGL0-3CRUISEPower….……………………………………….SET 55-75%Airspeed…..……….120-157KTS (<130KTS IN TURB.)DESCENTAltimeter…………………………………………………..SETFuel Selector………………………………FULLEST TANKPower Lever………………….AS REQUIRED FOR RODApproach Brief………………………………PLETE BEFORE LANDINGBrakes……………………………………………………..OFFFuel ………….………………………………QTY CHECKEDFuel Selector………………………………FULLEST TANK Fuel Pump……….………………………………BOTH (UP)LANDINGDOWNWINDAirspeed….………………………………………….90 KIASFlaps….………………………………………STAGE 1 (20°)Airspeed………….………………………………….65 KIASLanding Gear…..…………………….DOWN @ 65 KIASCHECK 3 GREENLanding Light………………………………………ON (UP)BASEFlaps…………………………… STAGE 2 (35°) < 65 KIASFINALAirspeed………….………………………………….60 KIASTouchdown ……………………….MAIN WHEELS FIRSTStick………………………………………………FULL BACK Brakes…………………………………………………..APPLYAFTER LANDING Flaps………………………………………………..RETRACT Landing Lights…………………………………………..OFFFuel Pump….………………………………MAIN (DOWN)SHUTDOWNParking Brake ……………………………………..ENGAGE Throttle……………………………………………………IDLE Switches….………………………….OFF EXCL. MASTERIgnition..…………………………………………………..OFFLights….……………………………………….OFF (DOWN)Master Switch..……………………………..OFF (DOWN)MEMORY ITEMS 2023 Orbx Simulation Systems Pty. Ltd For Microsoft Flight Simulator Use OnlyPROCEDURESIssued: 21 Apr 2023Revised: 21 Apr 2023。
V8完全傻瓜手册
V8完全傻瓜手册愿所有阅读过本文的爱好者，都能感受到V8的无穷乐趣，并能发扬大无畏的分享精神，共同壮大V8的队伍。
同时欢迎传阅，希望在黑暗中能点亮一片光明！---吾凡---版本号：V20100605目录1编写说明 (1)2V8的简介 (1)3傻瓜设置步骤 (2)3.1设置前准备 (2)3.1.1遥控器设置 (2)3.1.2V8和设备连接 (2)3.1.3安装4.0版本软件 (4)3.1.4V8和电脑连接 (4)3.1.5V8软件介绍 (4)3.1.6设置总体流程 (6)3.2进入设置阶段 (7)3.2.1步骤一预设（可跳过） (7)3.2.2步骤二遥控器校正 (9)3.2.3步骤三设置尾舵 (9)3.2.4步骤四设置十字盘舵机 (11)3.2.5步骤五设置十字盘水平 (13)4起飞前准备（重要） (15)5调整符合自己的手感 (15)5.1我要尾巴很爽很硬 (15)5.1.1来，先爽一下 (15)5.1.2爽完了，要硬的 (16)5.1.3又爽又硬，好，要射了 (17)5.2机体也需要爽硬啊 (18)6十万个为什么 (21)1编写说明本着服务大众，同欢同乐的原则以及怀着无比激动的心情，在咖啡和可乐的支持下，写下下面这些所谓傻瓜式的V8设置。
大体来说，本文适合下面几种人：¾没玩过，没接触过，没听过模型直升机的人。
¾玩过模型飞机，没玩过V8的初学者或者高手。
¾还在观望中，准备入V8的机友。
¾已经入了V8，但是一头雾水的兄弟。
¾入了V8并设置过，但是还是不明白的哥们。
手册只有两大部分内容：¾傻瓜设置步骤在这里，你可以按照里面的5个步骤，实现装上V8的飞机，可以飞行。
飞得好不好，我不能保证，但至少，能飞。
也就是说，设置V8，从0开始，只需要5个步骤。
读完并按照里面的步骤设置完后，飞机就可以起飞了。
¾调整符合自己的手感本部分内容，提供给需要进细节调整的同学。
SpaceWire总线节点控制器
Байду номын сангаас
SpaceWire 总线节点控制器 IP 核用户手册
目录
目 录........................................................................................................................................................ I
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3.2.1 控制寄存器（CTRL） ........................................................................................................29 3.2.2 状态寄存器（STATUS）.....................................................................................................31 3.2.3 节点地址寄存器（Node address） ....................................................................................32 3.2.4 时钟分频寄存器（Clock divider） ....................................................................................32 3.2.5 目的key寄存器（destination key）.....................................................................................32 3.2.6 时间寄存器（Time） ..........................................................................................................33 3.2.7 通道 1 DMA控制/状态寄存器（DMA channel 1 control/status）.....................................33 3.2.8 接收数据最大长度寄存器（DMA channel 1 rx maximum length） .................................34 3.2.9 发送描述符表地址寄存器（DMA channel 1 transmit descriptor table address） ...........35 3.2.10 接收描述符表地址寄存器（DMA channel 1 receive descriptor table address） ...........35 3.2.11 地址寄存器（DMA channel 1 address register）.............................................................35 3.2.12 接收描述符寄存器 0(receive descriptor word 0)..............................................................36 3.2.13 接收描述符寄存器 1(receive descriptor word 1)..............................................................36 3.2.14 发送描述符寄存器 0(transmit descriptor word 0)............................................................36 3.2.15 发送描述符寄存器 1(transmit descriptor word 1)............................................................37 3.2.16 发送描述符寄存器 2 (transmit descriptor word 2)...........................................................37 3.2.17 发送描述符寄存器 3 (transmit descriptor word 3)...........................................................38
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Java EE 5
ASCII XML Binary
Web Services
JCA
JMS Email SQL Hibernate JCA/Inflow Socket SOAP
Service Registry UDDI UDDI v3 Message Store Declarative Orchestration Engine BPEL BPEL jPDL
Questions: burr.sutter@
SOA Platform 4.2
Now Future Partners
Event Listeners and Actions provide transport mediation
Transports S HTTP(S) S
Pluggable Architecture
Service Clustering Stateful Fault Tolerance/Smart Load Balancing
Questions: burr.sutter@
App Server vs ESB for SOA
Accounting
Registry & Messaging
SOA Platform 4.2
Event Listeners and Gateways provide transport
mediation
Transports
Pluggable Architecture
for integrating infrastructure services
Business Services
Business Data
RDBMS Legacy COTS
Questions: burr.sutter@
ESB++ Scenario
HTTP FTP File JMS Email SOAP SQL Custom
HTTP FTP
jBPM
File JMS Email SOAP SQL Custom
for integrating infrastructure services
Business Services
runs within a container or standalone
FTP File
Business Service Components Infrastructure Services Transformation Routing Security Management
ASCII XML Binary
Web Services
JCA
JMS Email SQL Hibernate JCA/Inflow Socket SOAP
Service Registry UDDI Message Store Declarative Orchestration Engine BPEL jPDL
FTP File TCP
F I R E W A L L
Partners
Routing/Orchestration
.NET
Questions: burr.sutter@
Legacy
App Server vs ESB for SOA
ESB
Transformation
Java
REST JMS SOAP
Customer Inquiry Customer Inquiry Customer Update Customer Update Accounting Accounting
Transformation Services Cluster
* JVM
Questions: burr.sutter@
MQ
VPN
Web Service Web Service
ASCII
HQ (consumer & producer)
CC Auth
POS
(consumer)
DB Accounting Package
(consumer)
Reporting Engine
Questions: burr.sutter@
LAMP Registry & Messaging
FTP File TCP F I R E W A L L
Partners
Routing/Orchestration
.NET
Note: an ESB still runs in a JVM Legacy often that is an App Server
Questions: burr.sutter@
JBoss ESB 4.2
• JMX Microkernel • Federated Clustering • WS-* • • • – SOAP • – WSDL • – JAX-WS Annotated POJO Endpoints • – EJB Endpoints • – JAXB 2.0 BPEL 2.0 • New Deployment Architecture • .esb Archive • Hot Deployable Core Services • Content Based Filter Business Rules Services Native Process Orchestration Hibernate Gateway/Listener HTTP Gateway/Listener Groovy Scripting Declarative Message Store JCA Container Spring Action AOP & POJO Monitoring & Mgmt Tools Additional EIP examples
EJB Seam
ESB
POJOs Drools
Event Notification Custom Action
Spring Groovy
Service Component Architecture Service Data Object
Excel
Browser
Process Store
Web Native Java
JBoss SOA Platform 4.2 – Deep Dive
Burr Sutter
February 2008
App Server vs ESB for SOA
Servlet Servlet JMS JSP
RMI
JMS BPM
JSP
RMIEJB
EJB
WS SOAP/WSDL SOAP/WSDL JCA JCA
Questions: burr.sutter@
JBossESB 4.2 provides
• Message delivery
– – JMS (JBossMQ, JBoss Messaging, ActiveMQ, MQSeries, Oracle AQ, TIBCO EMS) FTP, SOAP, email, database, shared file system For custom service enablement & mediation XSLT, Java, Groovy, StringTemplate, Freemarker
run within a container or standalone
HTTP(S) (S)FTP File
Business Service Components Infrastructure Services Transformation Routing Security ManLeabharlann gementJava EE 5
Declarative Transformation includes: Message Normalization, Validation, Enrichment, Via XSLT, Groovy, Java, StringTemplate, FreeMarker
Business Data
RDBMS Legacy COTS
•
• • • • • • • •
Action chaining/pipeline
– –
Transformation Content-based routing
– –
– – –
JBoss Rules, XPath DSL Recipient List/Static Routing is also supported
Billing
Routing/Orchestration
CRM
Inventory
Questions: burr.sutter@
App Server vs ESB for SOA
Transformation
Java
REST JMS SOAP
LAMP Registry & Messaging
EJB Seam
ESB
POJOs Drools
Event Notification Custom Action
Spring Groovy
Service Component Architecture Service Data Object
Excel
Browser
Process Store
Web Native Java
Rules
J2EE/Java EE 5 Services
JMS EJB WS Hibernate JPA JCA
Questions: burr.sutter@
Service Federation
Warehouse Services
Shipping Calc Shipping Calc Shipping Calc Inventory Check Inventory Check Inventory Check Inventory Update Inventory Update Inventory Update