FIELD: transport.
SUBSTANCE: systems for automatic control of highly maneuverable aircraft flight provide required characteristics of longitudinal stability and controllability when aircraft is piloted at limit angles of attack and accelerations. The system contains sensor unit 1, automata 2 for longitudinal control with limit modes restrictor ("АПУ"), drive 3, functional unit 4, setting unit 5 for limit values of attack angles (acceleration), first multiplier 6, first adder 7, setting unit 8 for unit signal of allowed attack angle (acceleration) in the range of its limit values.
EFFECT: decrease in attack angle overcontrol in system virtually to zero which fact makes possible to improve significantly characteristics of longitudinal stability and controllability when aircraft is piloted at limit angles of attack and accelerations.
1 dwg
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