Investigation Possibilities of Creation of a Landing System for UAV Using Ultrasonic Altimeter
Remigijus Martynaitis
Abstract
The article discusses investigation of UAV landing systems, using ultrasonic altimeter. During investigation a UAV landing system model was designed, which used a navigation and height measurement system model. Errors of these systems, which can occur during the flight, were calculated. Model of calculation of errors is based on Kalman filter.
Article in Lithuanian
Article in:
Lithuanian
Article published:
2013-01-23
Keyword(s): UAV; ultrasonic altimeter; radio altimeter; barometric altimeter; inertia navigation system; GPS; Kalman filter
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