FIELD: physics, navigation.
SUBSTANCE: invention relates to radar and simulation-testing systems designed to evaluate properties of radar objects. The simulation-testing system for a radar station comprises a target for creating a full-scale environment in a field of view according to a given fly-by program. On-board the target there is a pilot-navigation system, connected to a satellite navigation system, and a measuring electronic device, both connected to a control station. The target is an unmanned aerial vehicle (UAV). The UAV comprises a wing, a tail unit, a fuselage, an engine and landing gear. The launch apparatus comprises a guide which is mounted with a pusher and a removable extensible stator on the side of the engine propeller. A support is mounted on the fuselage in its lower part on a longitudinal axis, said support being in contact with the end surface of the pusher at take-off. The landing gear of the UAV is installed in a compartment, on the wall of which an opening flap, which is connected to an automatic key, is mounted.
EFFECT: simple tests, improved operation and transportation conditions, enabling investigation of different types of radar stations at deployment sites without the necessary equipment.
6 cl, 5 dwg
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Authors
Dates
2014-11-20—Published
2012-09-11—Filed