en:uav
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| + | ====== Experimental construction of Unmanned Aerial vehicle ====== | ||
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| + | ===== " | ||
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| + | {{: | ||
| + | |||
| + | ==== Major improvements ==== | ||
| + | |||
| + | * More reliable bus infrastructure (CAN) | ||
| + | * More volume and weight capacity for experimental avionics and payload | ||
| + | * Adding additional control layer realised by powerfull ARM computer [[en: | ||
| + | |||
| + | |||
| + | ===== Flying wing " | ||
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| + | {{: | ||
| + | |||
| + | |||
| + | ==== Airframe ==== | ||
| + | |||
| + | === Mechanical Construction === | ||
| + | |||
| + | |||
| + | === Virtual mathematical model === | ||
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| + | |||
| + | ==== Control System ==== | ||
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| + | {{: | ||
| + | |||
| + | === Required features === | ||
| + | |||
| + | * 10Hz update rate | ||
| + | * Airspeed (min 16m/s, avg 22,3 m/s, max 30m/s) 600Pa max | ||
| + | * Barometer (Air density, altitude) | ||
| + | * Humidity sensor (Fail safe, Air density) | ||
| + | * Temperature sensor (Fail safe, Air density) | ||
| + | * Camera? | ||
| + | * Battery Voltages, Currents (Battery gas gauge) | ||
| + | * Engine power sensing, max engine current 30A. | ||
| + | * GPS | ||
| + | * IMU (Akcelerometers -3G to 5G) | ||
| + | * Magnetometer | ||
| + | |||
| + | |||
| + | === Hardware === | ||
| + | |||
| + | == Non fly prototype == | ||
| + | |||
| + | Non fly prototype is build from [[http:// | ||
| + | |||
| + | {{: | ||
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| + | == CPUs == | ||
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| + | PPM Decoder/ | ||
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| + | Main UAV control board is based on [[http:// | ||
| + | |||
| + | == Sensors == | ||
| + | |||
| + | == IAS == | ||
| + | |||
| + | * [[http:// | ||
| + | |||
| + | == GPS == | ||
| + | |||
| + | * [[cs: | ||
| + | * [[http:// | ||
| + | |||
| + | == Current and Voltage sensor == | ||
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| + | Resistive current measurement sensor with analog output and voltage divider to 3,3V range [[cs: | ||
| + | |||
| + | == Altitude measurement == | ||
| + | |||
| + | Barometric [[cs: | ||
| + | |||
| + | == Absolute terain altimeter == | ||
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| + | Absolute terrain altimeter is necessary for correct landing procedure. It can be resolved by several methods laser, ranging, radar ranging, camera terrain angle speed measurement, | ||
| + | |||
| + | We would use the simplest sonar ranging method at beginning. | ||
| + | |||
| + | == IMU == | ||
| + | |||
| + | Inercial measurement unit is based on [[cs: | ||
| + | |||
| + | == Magnetometers == | ||
| + | |||
| + | Magnetic orientation will be measured by two redundant magnetic sensors modules [[cs: | ||
| + | |||
| + | === Telemetry === | ||
| + | |||
| + | Telemetry will be realized by UART ascii output in NMEA like format. [[http:// | ||
| + | |||
| + | Another considered variant is use of some more powerfull telemetry modules [[http:// | ||
| + | |||
| + | === Data logging === | ||
| + | |||
| + | Measured data will be stored in SD card. [[cs: | ||
| + | |||
| + | |||
| + | === Radio Control === | ||
| + | |||
| + | We will use the JETImodel RC receiver [[http:// | ||
| + | |||
| + | ==== Software ==== | ||
| + | |||
| + | === Ideas === | ||
| + | |||
| + | == linear algebra == | ||
| + | | ||
| + | | ||
| + | |||
| + | == realtime OS: == | ||
| + | |||
| + | * [[http:// | ||
| + | * [[http:// | ||
| + | |||
| + | Bachelor' | ||
| + | |||
| + | === Testing === | ||
| + | |||
| + | The autopilot software control algorithm will be tested by [[http:// | ||
| + | |||
| + | |||
| + | ====== Ground control station ====== | ||
| + | |||
| + | Provedeni DGPS: | ||
| + | Pozemni stanice bude vysilat vlastni telemetrii, ktera bude obsahovat DGPS korekce. Ty se v UAV pouziji pro vypocet polohy, ktera se opet telemetrii odesle do pozemni stanice. | ||
| + | Navigace tak bude v podstate rozdilova proti pozemni stanici. | ||
| + | To umozni snazsi definovani bodu trasy a nasledne i pripadne zjednodussi budouci moznost pristavani pobliz pozemni stanice. | ||
| + | |||
| + | |||
| + | ==== Hardware ==== | ||
| + | |||
| + | === Datalinks === | ||
| + | |||
| + | * [[http:// | ||
| + | |||
| + | === Programmers === | ||
| + | |||
| + | * [[http:// | ||
| + | |||
| + | |||
| + | ====== Documentation ====== | ||
| + | |||
| + | ===== Technical documentation ===== | ||
| + | |||
| + | Project files are stored in [[svn:// | ||
| + | |||
| + | In Ubuntu run this command to check out all project documents. | ||
| + | |||
| + | svn co svn:// | ||
| + | | ||
| + | ===== Project management ===== | ||
| + | |||
| + | For tasks management and supervision of their implementation we use [[http:// | ||
| + | |||
| + | |||
| + | ====== Administrative ====== | ||
| + | |||
| + | ==== People ==== | ||
| + | |||
| + | * Ivan Jerabek | ||
| + | * Jakub Kákona - kaklik@mlab.cz | ||
| + | * Marian Such | ||
| + | * . | ||
| + | * . | ||
| + | * . | ||
| + | |||
| + | |||
| + | ==== External links ==== | ||
| + | |||
| + | Other similar known projects for reference: | ||
| + | |||
| + | * [[http:// | ||
| + | * [[http:// | ||
| + | * http:// | ||
| + | * http:// | ||
| + | * http:// | ||
| + | * http:// | ||
| + | * http:// | ||
| + | * http:// | ||
| + | * http:// | ||
| + | |||
| + | === Partners of project === | ||
| + | |||
| + | Project is supported by [[http:// | ||
| + | |||
| + | ==== Law & legal issues regarding UAV ==== | ||
| + | |||
| + | [[Legislativa|Model parameters and radio transmissions limits]] (cz only) \\ | ||
| + | [[http:// | ||
| + | |||
| + | |||
en/uav.txt · Last modified: 2013/11/01 01:09 (external edit)
