000			02270nam a22002417a 4500
003			OSt
005			20241003162026.0
008			240816b |||||||| |||| 00| 0 eng d
040			_cFoundation University
050			_aLG 221 D35 C66 _bA5 C66 2017 V366
100			_aVan Stone, Jamie Joe M. _97594
245			_aDrone stabilization system based on kalman and proportional-integral-derivative algorithms [thesis] / _cJamie Joe M. Van Stone, Jassam Alinsub, and Jeffrey Tubog.
260			_aDumaguete City: _bFoundation University; _c2017
300			_avii, 71 leaves : _bill. (col.) _c275 cm.
502			_6Thesis Undergraduate (BS Computer Science) -- Foundation University, 2017
504			_aIncludes bibliographical references and appendices.
520			_aA multi rotor copter is a rotorcraft with more than two rotors. A typical multi rotor copter has around 4 rotors. These devices are mainly controlled by a radio controller or a wifi controller. They are supported by a flight controller which handled most of the balancing and output for the commands from controllers. Flight controllers are a powerful piece of technology since they are able to compute data quickly and provide a precise response which in return greatly improve the experience of flying the devices. Most flight controller include a gyroscope and accelerometer to gather data about the devices orientation during flight which then would be computed to an output for the rotors. The same can be achieved using other components such as a micro controller and an Inertial Measurement Unit. This study aims to provide a learning basis to develop flight controllers using available components such as GizDuino microcontroller, GizDueno Bluetooth Sheild, an Sparkfun IMU, an android device and a quad copter. The results show that that it may be possible to develop a flight controller with such components however the accuracy results have come out below satisfactorily due to the time constraints to conduct tests.
650			_2LC _aDrone _98317
658			_aThesis Writing 2 _bComputer Science. Bachelor of Science _cCS 416
690			_2FU _aflight control _98318
690			_2FU _aDrone _98317
942			_2lcc _cTH _n0 _hLG 221 D35 C66 _iA5 C66 2017 V366
999			_c3506 _d3506