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Navigation Guidance and Control System using Hardware in the Loop Simulation for Unmanned Aerial Vehicle ( UAV )
| Content Provider | Semantic Scholar |
|---|---|
| Author | Maung, Thae Maung Naing, Moe Kyaw |
| Abstract | Field trial is very critical and high risk in autonomous UAV development life cycle. Hardware in the loop (HIL) simulation is a computer simulation that has the ability to simulate UAV flight characteristic, sensor modeling and actuator modeling while communicating in real time with the UAV autopilot hardware. HIL simulation can be used to test and validate the UAV autopilot hardware reliability, test the closed loop performance of the overall system and tuning the control parameter. By rigorous testing in the HIL simulator, the risk in the field trial can be minimized in research and development UAV autopilot. This paper presents a practical approach of applying an Inertial Navigation System (INS) using MEMS inertial sensors, Global Positioning System (GPS) receiver for the Guidance, Navigation and Control (GNC) of an autonomous Unmanned Aerial Vehicle (UAV). And the HIL environment can give the best results by comparing with practical unmanned fight test. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://psrcentre.org/images/extraimages/47.%201011166.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
