Telemetric system for increasing safety of ultralight airplane operation

摘要

The telemetric system according to the present invention comprises a commonly used device (1) EFIS with external sensors and an external computation unit (2). The external computation unit (2) consists of a trajectory spatio-temporal organizer (2.5) connected to a block of static field map block (2.3), a static map bases block (2.4), a decoder (2.2) of a navigation actual target, interpreter (2.1) of the airplane actual state in the space and a decoder (2.8) of flight trajectory collisions, in which its output is connected, too, as well as in the second collision decoder (9.8). The interpreter (2.1) inputs are the GPS navigation system (5) and an internal sensory unit (1.2). The decoder (2.2) input is the GPS navigation system (5). The other collision decoder (2.8) inputs are a flight trajectory predictor (2.7) and a second spatio-temporal organizer (9.5), whereby the output is connected to a breakaway maneuver organizer (2.9). Said breakaway maneuver organizer (2.9) output is connected to a breakaway trajectory evaluator (2.10), which is at the same time the input thereof. The breakaway trajectory evaluator (2.10) is connected to a breakaway trajectory applicator (2.11) having its output connected to a second applicator (9.11) and to a visualization system (1.3). The flight trajectory predictor (2.7) makes use of its input receiver (3) ADS-B and an absolute position decoder (2.6) having on its input the interpreter (2.1) and the CAS system (4). Wireless communication devices (7, 10) serve for connection with a second computation unit (9) of a cooperating airplane.