COLLISION AVOIDANCE SYSTEM FOR FLIGHT TESTS Russian patent published in 1999 - IPC

FIELD: aeronautical engineering. SUBSTANCE: system designed for mounting on board aircraft has altitude-speed signal metering subsystem, input adapter, output adapter, central computer incorporating constants input unit, device computing parameters of relative position of flying vehicles, actual coordinate computer, aircraft-to-aircraft range computer, data pre-processing computer, relative speed computer, dangerous approach area identifying computer, and common time front computer, as well as data display and warning subsystems, automatic control subsystem and thrust controller, satellite navigation subsystem, inertial navigation subsystem, aircraft-to-aircraft exchange subsystem, and coupling controller. In addition, system includes ground monitoring and correcting station and flying experiment control station; coupling controller of flying vehicle is coupled with monitoring and correcting station through radio equipment; flying experiment control station is coupled through radio equipment with aircraft-to-aircraft exchange equipment. EFFECT: improved accuracy and safety during flight tests. 2 cl, 4 dwg