Auxiliary monitoring device in flight control system

A monitoring device and aircraft technology, applied in the control/regulation system, non-electric variable control, three-dimensional position/course control, etc., can solve the problems of heavy driving tasks, heavy physical exertion of crew members, etc., and achieve the goal of improving operational safety Effect

Active Publication Date: 2018-10-30
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The existing problems are: the crew pilots are responsible for the formulation of specific flight tasks, various stages of flight control, instrumentation monitoring, etc., and undertake relatively heavy driving tasks, especially in international long-distance flights, the crew pilots are physically exhausted
[0005] The current aircraft lacks a long-term effective auxiliary monitoring measure for driving during flight. It is precisely because of the lack of a long-term effective auxiliary monitoring measure during flight that flight accidents caused by pilots' unintentional or malicious manipulation often occur.

Method used

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  • Auxiliary monitoring device in flight control system
  • Auxiliary monitoring device in flight control system

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Embodiment 1

[0015] The functional principle of an auxiliary monitoring device in a flight control system is as follows: figure 2 As shown, the workflow is as follows image 3 shown. The core processing module (computer) mainly includes key components such as database unit, processing unit, recording unit, sending unit and alarm unit. The database unit stores a large amount of rule data that violates flight regulations, including: flight routes entering no-fly zones, abnormal deviations of actual routes, abnormal responses to air traffic control instructions, etc., as well as unsafe flight control data, including: large-scale attitude Maneuvering, heavy landing, tail strike, etc. There are two working modes in the processing unit: image-based voice mode and avionics network-based mode.

[0016] In the image-based voice mode, the authorized personnel operation information and air traffic control instruction information received through the human-computer interaction touch panel, as well...

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Abstract

The invention relates to the field of flight control systems, in particular to an auxiliary monitoring device in a flight control system. The auxiliary monitoring device comprises a core processing module; the core processing module comprises a database unit, a processing unit and a sending unit; rule data violating flight regulations and unsafe flight control data are stored in the database unit,the processing unit acquires a real-time flight airway and attitude information of an aircraft, the real-time flight airway and attitude information of the aircraft and the rule data violating the flight regulations and the unsafe flight control data are compared and analyzed, once the real-time flight airway and attitude information of the aircraft and the rule data violating the flight regulations and the unsafe flight control data are anastomotic, anastomotic information is transmitted to the sending unit; and the sending unit transmits the anastomotic information to a ground blank pipe. The auxiliary monitoring device in the flight control system has the advantages that through the effective combined design of flight status information of the aircraft and active perception informationof the system, the flight is monitored in real time, it is achieved that effective supervision and alarm of driving are provided for flight crews, and the occurrence of flight accidents caused by man-made operation is avoided.

Description

technical field [0001] The invention relates to the field of flight control systems, in particular to an auxiliary monitoring device in the flight control system. Background technique [0002] The flight control system of an aircraft is generally composed of the main flight control system, high-lift system and automatic flight control system, and the manipulation of these systems is realized by the pilot crew. In the field of civil aircraft, the cockpit control crew is generally composed of a pilot and a co-pilot. Usually, the captain on the left completes the key actions in the take-off and landing phases. The co-pilot usually helps to complete the checklist and check whether the instruments are normal. Assists in retracting flaps and landing gear. The pilot and the co-pilot are axisymmetric, and the control mechanisms on both sides are exactly the same. The handle for controlling the throttle is in the middle, and both the pilot and the co-pilot can control it. [0003] ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10B64D47/02G06F17/30
CPCG05D1/101B64D47/02
Inventor 白志强徐舒寒陈少敏赵广涛李喜玉
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC
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