Design aspects of flight and navigation systems for small UAVs of different types
| Autor: | E. N. Scripal, R. V. Ermakov, A. A. Seranova, D. Yu. Livshits, D. E. Gutsevich, I. V. Sergushov, S. N. Romadin, A. V. Abakumov |
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| Rok vydání: | 2017 |
| Předmět: |
010504 meteorology & atmospheric sciences
Computer science 010401 analytical chemistry Flight inspection Flight management system Navigation system ComputerApplications_COMPUTERSINOTHERSYSTEMS Ground control station Control engineering 01 natural sciences Flight simulator Fly-by-wire 0104 chemical sciences Air navigation Flight control modes 0105 earth and related environmental sciences |
| Zdroj: | 2017 24th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS). |
| DOI: | 10.23919/icins.2017.7995617 |
| Popis: | The main problems in developing flight and navigation systems for small unmanned aerial vehicles (with the takeoff weight not exceeding 100 kg) and their possible solutions are considered. An example of a flight and navigation system construction for a helicopter-type aerial vehicle is given. The following aspects are considered: hardware implementation of the flight control computer, implementation of the ground control station and aircraft stabilization algorithms. The choice of sensors used to obtain primary information is substantiated. The results of the flight tests are discussed. |
| Databáze: | OpenAIRE |
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