FIELD: aeroplanes; helicopters
SUBSTANCE: The invention relates to a method for automatic of homing manned and unmanned aerial vehicles (UAVs) on hypersonic aircraft (HPLA). For homing aircraft on a guided aircraft, a control signal ji is formed according to a certain law, taking into account the angle of sight of the target, the speed of its change, the time constant of the control object according to the angular velocity of the course, the efficiency coefficient of the interceptor, the pitch angles of the target and the interceptor, respectively, the coefficients determined by the solution of a certain system of algebraic equations. In addition, the balancing value of the overload j03 is calculated at steady-state flight modes, taking into account the target maneuver according to a certain law, taking into account the angles of sight and the speed of its change, the efficiency coefficients of the interceptor and the target, the time constant of the object according to the angular velocity of the course. Based on the calculated values, control signal ji=jn+j03 is formed, which is transmitted to the interceptor's SPG to change its trajectory relative to the target.
EFFECT: optimal aircraft control signal is generated.
1 cl, 6 dwg
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Authors
Dates
2021-07-13—Published
2020-03-25—Filed