INTEGRATED FAULT-TOLERANT ALTITUDEMEASURING SYSTEMFOR AN UAV |
| 4 | |
| 2010 |
| scientific article | 681.586.325 | ||
| 146-152 | unmanned aerial vehicle (UAV), control system, inertial navigation system, radio altimeter, data protection, information security, the Kalman filter |
| The paper treats the integrated altitude measuring system synthesis for an UAV low-altitude flight support, the
measuring system being protected against radio altimeter faults and invalid data. A method for the radio altimeter
measurement data monitoring is proposed. The delayed Kalman filter is implemented, and an adjustment of the
integrated altitude measuring system is performed. Simulation results demonstrating the efficiency of the proposed
method are given. |
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