FIELD: aviation.
SUBSTANCE: invention relates to measurement information systems and combat aircraft systems. Proposed method of forming air-speed parameters of manoeuvrable object consists in combined processing of information, including current values of air speed and angles of attack and sliding modules, which are measured by system of air signals and sensor of angles of attack and sliding, orientation of object relative to coordinate system, current design value of wind velocity module, as well as unknown to be evaluated functional parameters formed by results of inertial-Doppler correction of angles of true course, bank and pitch of object and module of track speed of object with determining its current spatial orientation relative to own coordinate system.
EFFECT: broader functional capabilities of modern aviation equipment and high accuracy and efficiency of its piloting and combat employment in all operating conditions.
1 cl, 11 dwg
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Authors
Dates
2020-02-05—Published
2019-01-29—Filed