Flying method and system using total power for an aircraft

Details Flying method and system using total power for an aircraft Flying method and system using total power for an aircraft

G - Physics

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G06G 7/78 (2006.01) B64C 13/50 (2006.01) G05D 1/00 (2006.01) G05D 1/06 (2006.01)

Patent

CA 1088655

ABSTRACT OF THE DISCLOSURE A flying method using total energy, in particular for the take-off and overshoot of an aircraft, is disclosed in which the aerodynamic flight path angle .gamma. a is governed by reference to a desired flight path angle .gamma. d which is the potential flight path .gamma. t modulated by the difference between the aircraft speed V and a reference speed V2. An error signal .delta. representative of the difference between the aerodynamic flight path angle .gamma. a and the desired flight path angle .gamma. d is displayed. The display of the desired flight path angle .gamma. d may be by means of the pitch com- mand bar of an attitude director indicator for example.

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