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The autothrottle subsystem was designed for a fly-by-wire control system for a small commercial aircraft. Classical control laws were used to control aircraf indicated airspeed, Mach number or thrust within the full flight envelope. The autothrottle blocks developed in Simulink were included into a computer model of an aircraft flight control system ond tested both in computer simulations alone and...
Autopilot in fly-by-wire control system was developed for small commercial aircraft. Longitudinal control modes of autopilot are described in this paper.
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