The invention discloses a semi-physical
simulation system and method for a gliding extended-range guided aircraft. The
simulation equipment comprises a rolling
motion simulation turntable
system, an electric steering engine load
simulation system, a sensor measurement system, an information setting module, a gliding extended-range guidance aircraft trajectory calculation module, a data communication module, a
data display and
system evaluation module and the like.
Missile-borne test parts comprise a
missile-borne flight control computer and the like. The information setting module sets trajectory initial information and pulling deviation information, and the gliding extended-range guided aircraft trajectory resolving module calculates aircraft trajectory information and sends the aircraft trajectory information to the rolling
motion simulation turntable system, the electric steering engine load
simulation system and the
missile-borne flight control computer; the
missile-borne flight control computer performs
trajectory control according to a preset control strategy to obtain a lift airfoil angle control instruction, and the lift airfoil angle control instruction is controlled to a
target angle by a double-rotation electric steering engine; the
data display and evaluation module collects related simulation and
control data, and evaluates, detects and optimizes missile-borne tested parts.