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Aircraft cockpit man-machine function distribution method based on load balancing

A technology of load balancing and function distribution, applied in the direction of computer components, mechanical mode conversion, data processing input/output process, etc., which can solve the lack of effective technical means for dynamic function distribution decision-making and the inability to adapt to the new requirements of the intelligent development of the system , The development of dynamic function allocation method is not mature, etc.

Pending Publication Date: 2020-10-13
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

Among them, the static function allocation method has become mature, but it cannot adapt to the new requirements of the intelligent development of the system; the development of the dynamic function allocation method is not yet mature, and there is a lack of effective technical means to support dynamic function allocation decision-making

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  • Aircraft cockpit man-machine function distribution method based on load balancing
  • Aircraft cockpit man-machine function distribution method based on load balancing
  • Aircraft cockpit man-machine function distribution method based on load balancing

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Embodiment Construction

[0057] The present invention will be further explained below in conjunction with the accompanying drawings and specific embodiments. The embodiments described in the present invention are only some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, other embodiments obtained by persons of ordinary skill in the art without creative efforts all belong to the protection scope of the present invention.

[0058] The present invention is a method for allocating man-machine functions in an aircraft cockpit based on load balancing, comprising the following steps:

[0059] (1) Carry out flight mission analysis based on different flight scenarios that may occur in each flight phase of a certain flight mission;

[0060] (1.1) Define the overall goal of a certain flight mission, which can be to complete a mission from takeoff to landing, or to complete a go-around during approach;

[0061] (1.2) Design the flight scenario...

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Abstract

The invention discloses an aircraft cockpit man-machine function distribution method based on load balance, which comprises the following steps: analyzing the task load of a pilot for a flight task, and analyzing the flight task complexity based on an entropy method; establishing a pilot task load quantification model by integrating pilot task complexity and physiological and psychological characteristics; aiming at the functional characteristics of the airplane cockpit man-machine system, determining an automation level set of an airplane cockpit airborne system; with pilot task load balanceas a target, an aircraft cockpit airborne system automation level dynamic adjustment model is established based on a fuzzy algorithm, and achieving coordination of an aircraft cockpit man-machine system in a dynamic environment. The method has important significance and application value for improving task scene adaptability, response timeliness and flight safety of a future intelligent aircraft cockpit man-machine system.

Description

technical field [0001] The invention belongs to the technical field of complex human-machine system design, and in particular relates to a method for allocating human-machine functions in an aircraft cockpit based on load balancing. Background technique [0002] Aircraft cockpit man-machine function allocation refers to the assignment of functions or tasks in the aircraft cockpit man-machine system to the pilot or the cockpit airborne system. Man-machine function allocation methods can be divided into static function allocation and dynamic function allocation. Static function allocation is the function allocation between man and machine through the comparison and analysis of human-machine capabilities at the beginning of system design. Once determined, it will not change; and dynamic function allocation Function allocation refers to the dynamic adjustment of the function allocation between man and machine according to the actual operating status of the system, so as to achie...

Claims

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Application Information

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IPC IPC(8): G06F30/15G06F30/20G06F3/01G06F17/10G06Q10/06
CPCG06F30/15G06F30/20G06F3/015G06F17/10G06Q10/063112
Inventor 孙有朝孙丽
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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