Variable human-sensing control system

A control system and variable technology, applied in the direction of instruments, simulators, space navigation equipment, etc., can solve problems such as low safety, and achieve the effect of improving the quality level and shortening the training time.

Pending Publication Date: 2022-03-11
南京航旭机电设备有限公司
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Problems solved by technology

The human-sensing system of the aircraft has gone through a series of development processes. The design of t

Method used

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Embodiment Construction

[0034] It is easy to understand that, according to the technical solution of the present invention, those skilled in the art can propose multiple structural modes and implementation modes that can be replaced without changing the essence and spirit of the present invention. Therefore, the following specific embodiments and drawings are only exemplary descriptions of the technical solution of the present invention, and should not be regarded as the entirety of the present invention or as a limitation or restriction on the technical solution of the present invention.

[0035] Such as Figure 2-3 As shown, as an embodiment of the present invention, the present invention provides a technical solution: a variable human-sensing control system, including a human-sensing computer, force sensors connected to the human-sensing computer, displacement sensors, servo valves, actuators and Rod force device, wherein,

[0036] The force sensor is used to measure and feedback the actual rod f...

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Abstract

The invention provides a variable human-sensing control system, which comprises a human-sensing computer, and a force sensor, a displacement sensor, a servo valve, a driver and a rod force device which are respectively connected with the human-sensing computer, and is characterized in that the force sensor is used for measuring and feeding back the actually applied rod force; the displacement sensor is used for measuring rod force displacement and establishing information interaction feedback of flight control regulation and control with the human sensing computer; and the servo valve is used for performing control output on the human sensing computer and performing information conversion so as to serve as execution component output for pressure regulation of the human sensing control system. Nonlinear characteristics such as starting force of an aircraft control system are simulated, and dynamic characteristics such as rod force gradient of a control mechanism are simulated; therefore, the aim of carrying out air flight simulation on the human feeling characteristics of the researched object is fulfilled, and the method has the advantages of shortening the training time of the pilot on the actual airplane and improving the quality level of the pilot.

Description

technical field [0001] The invention relates to the technical field of aircraft on-board systems, in particular to a variable human touch control system. Background technique [0002] The variable human sense system is the core airborne equipment of the aircraft airborne system and a key part of improving the flight ability of the aircraft pilot. The human sensor system of the aircraft has gone through a series of development processes. The design of the early mechanical flight control system was very simple, and the safety was low, which has become a history. The current human sensor system is developing relatively slowly and has become a shortcoming in the mature composite flight control system. It is known that half of the global flight accidents are caused by aircraft errors during flight, which lead to tragedies. Therefore, how to improve the relative performance of the human sensor system is one of the important means to improve the pilot's flying ability. [0003] B...

Claims

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Application Information

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IPC IPC(8): G09B9/28
CPCG09B9/28
Inventor 曹伟
Owner 南京航旭机电设备有限公司
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