KR101298779B1 - Integrated test system for supporting multiple forms of aircraft and mehtod for controlling that system - Google Patents

Abstract

The present invention has been made in an effort to provide an integrated experimental system for supporting an aircraft multi-shape and a method of controlling the system, which supports a derivative aircraft, instead of an experimental system supporting a single shape of an aircraft.
According to an aspect of the present invention, there is provided an integrated laboratory for aircraft support, comprising: a power supply unit supplying power to aircraft equipment mounted to the integrated laboratory; A power control unit controlling power supplied from the power supply unit to the aircraft equipment; A signal controller for controlling data signals transmitted and received between several aircraft equipment; And a first shape control unit controlling the power control unit and the signal control unit. Provided is an integrated experimental system for supporting an aircraft multi-shape comprising: (a) receiving an aircraft shape to be implemented in an integrated laboratory; (b) reading a control database for the aircraft shape received in step (a); And (c) controlling the power control unit and the signal control unit according to any one of claims 1 to 4 from the first shape control unit according to any one of claims 1 to 4, and inputting in the step (a). Constructing the received aircraft shape; Provided is a method of controlling an integrated experimental system for supporting aircraft multi-shape support.
As a result, it is possible to expand from a single-shaped aircraft support experimental system to a multi-shaped aircraft support experimental system, thereby preventing the increase in the cost and length of time required for development and manufacturing in the existing single-shaped aircraft support experimental system, and It is easy to add and delete the equipment of the supporting experimental system by using the shape control software, and it is easy to set up and use the environment that the operator wants to use, so it is excellent in scalability and when adding and deleting the equipment of the aircraft supporting experimental system. Easy to configure aircraft shape without affecting other equipment.

Description

Integrated test system for aircraft multi-shape support and control method {INTEGRATED TEST SYSTEM FOR SUPPORTING MULTIPLE FORMS OF AIRCRAFT AND MEHTOD FOR CONTROLLING THAT SYSTEM}

The present invention relates to an integrated laboratory for supporting aircraft multi-shape, and more specifically, a system capable of simultaneously supporting a derivative aircraft business that will occur in the future during aircraft development, thereby achieving an effect of preventing overlapping investment and shortening development time. To control the system.

An integrated experimental system is a support system developed for the purpose of finding a fault by establishing an environment similar to an aircraft before installing hardware on the aircraft.

In the aircraft development project, the integrated experimental system generally develops and manufactures one system on a project basis in consideration of the production cost and schedule of the system. This is because the cost of the aircraft equipment to be installed is expensive and the shape of the aircraft to be supported during development is often single.

Integrated experimental systems developed to support single-shaped aircraft cannot support derived aircraft in the event of a derivative project. In addition, if the development period is short, it is difficult to develop and manufacture additional experimental systems.

Therefore, there is an urgent need for a system capable of supporting a derivative aircraft in which an additional generation is expected, in addition to a system capable of supporting an initially planned aircraft through the development of an integrated experimental system for supporting multiple shapes.

Accordingly, the technical problem to be achieved by the present invention is to provide an integrated experimental system for supporting an aircraft multi-shape to support a derivative aircraft and a method for controlling the system, away from the experimental system for supporting a single shape of the aircraft.

As a means of the present invention for achieving the above object, in an integrated laboratory for aircraft support, a power supply unit for supplying power to the aircraft equipment mounted to the integrated laboratory; A power control unit 200 controlling power supplied from the power supply unit 100 to the aircraft equipment; A signal controller 300 for controlling data signals transmitted and received between several aircraft equipment; And a first shape control unit 400 controlling the power control unit 200 and the signal control unit 300. Provides an integrated experimental system for supporting aircraft multi-shape comprising.

In addition, the power control unit 200 and the signal control unit 300 provides an integrated experimental system for supporting aircraft multi-shape, characterized in that consisting of a mechanical or electronic relay circuit.

In addition, the second shape control unit 500 for detecting whether the aircraft equipment is mounted / detached; It provides an integrated experimental system for supporting the aircraft multi-shape further comprising.

In addition, when the second shape control unit 500 is connected to the aircraft equipment, the integrated test for supporting the aircraft multi-shape, characterized in that whether to detect the mounting / detachment of the aircraft equipment through the ground recognition through the aircraft equipment. Provide a system.

In addition, (a) the control unit 10, receiving an aircraft shape to be implemented in the integrated laboratory; (b) reading, by the controller 10, a control database for the aircraft shape input in the step (a); And (c) the controller (10) controlling the power controller (200) and the signal controller (300) by the first shape controller (400) to configure an aircraft shape input in the step (a); It provides a method for controlling an integrated experimental system for supporting aircraft multi-shape comprising.

In addition, between the step (b) and the step (c), (A) the second shape control unit 500 detects whether or not the equipment for the aircraft; And (b) the control unit 10, comparing the input control database with the configuration of the aircraft equipment detected in the step (a) and notifying the operator if there is a mismatch; It provides a method for controlling an integrated experimental system for supporting aircraft multi-shape further comprising.

In addition, in the step (a), the second shape control unit 500 detects whether the aircraft equipment is mounted or detached through ground recognition through the aircraft equipment when the second shape controller 500 is connected to the aircraft equipment. It provides a method for controlling an integrated experimental system for supporting aircraft multi-shape.

According to the present invention, it is possible to expand from a single-shaped aircraft support experimental system to a multi-shaped aircraft support experimental system, thereby preventing the increase in the cost and length of time required for development and manufacturing in the existing single-shaped aircraft support experimental system. can do.

In addition, according to the present invention, the equipment of the aircraft support experimental system can be easily added and deleted using the shape control software, the operator can easily set the environment to use, excellent in terms of scalability.

In addition, according to the present invention, when adding and deleting equipment of the aircraft support experimental system does not affect other equipment, it is easy to configure the aircraft shape.

In addition, according to the present invention, since the aircraft equipment can be automatically recognized, it is possible to prevent some of the equipment for a number of aircraft missing or incorrectly connected in advance.

1 is a view schematically showing a conceptual diagram of a laboratory for supporting aircraft multi-shape according to an embodiment of the present invention,
FIG. 2 is a diagram briefly showing a configuration of controlling power and communication signals between respective devices of an experimental system for supporting an aircraft multi-shape according to an embodiment of the present invention.
3 is a diagram illustrating a mutual relationship in which a second shape control unit included in a control unit detects aircraft equipment according to an embodiment of the present invention.
4 is a diagram illustrating a method of controlling an experimental system for supporting an aircraft multi-shape according to an embodiment of the present invention.

The following detailed description of the invention refers to the accompanying drawings, which illustrate, by way of illustration, specific embodiments in which the invention may be practiced. These embodiments are described in sufficient detail to enable those skilled in the art to practice the invention. It should be understood that the various embodiments of the present invention are different, but need not be mutually exclusive. For example, certain shapes, structures, and characteristics described herein may be embodied in other embodiments without departing from the spirit and scope of the invention in connection with one embodiment. It is also to be understood that the position or arrangement of the individual components within each disclosed embodiment may be varied without departing from the spirit and scope of the invention. The following detailed description is, therefore, not to be taken in a limiting sense, and is defined only by the appended claims, along with the full scope of the present invention, and all equivalents to which the claims are entitled. In the drawings, like reference numerals refer to the same or similar functions throughout the several views.

Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings, so that those skilled in the art can easily carry out the present invention.

1 is a view schematically showing a conceptual diagram of a laboratory for supporting aircraft multi-shape according to an embodiment of the present invention.

As shown in Figure 1, the integrated experimental system for supporting aircraft multi-shape of the present invention is largely supplied to the aircraft equipment from the power supply unit 100, the power supply unit 100 for supplying power to the aircraft equipment mounted in the integrated laboratory A power control unit 200 for controlling the power to be controlled, a signal control unit 300 for controlling data signals transmitted and received between the aircraft equipment, and a first shape control unit for controlling the power control unit 200 and the signal control unit 300 400.

Due to the nature of the aircraft business, mass production, export, and derivative business is inevitable, and if the shape of the aircraft changes according to the characteristics of the business at this time, it is impossible to support all of these multi-shape aircraft in time and cost with a single laboratory. .

Therefore, in the present invention, in order to construct an integrated experimental system for supporting an aircraft having a multi-shape, to equip an aircraft equipped with the aircraft, and to build an environment suitable for the shape of the aircraft, power control for the aircraft equipment And a power control unit 200 and a signal control unit 300 connected to the first shape control unit 400 for signal control.

At this time, the power control unit 200 and the signal control unit 300 is controlled through the first shape control unit 400, each preferably composed of a mechanical or electronic relay.

That is, when the equipment is changed in preparation for the basic shape aircraft through the first shape control unit 400, the integrated laboratory for the aircraft of various shapes can be easily set and used by supplying or cutting off the power and signals of the equipment.

In addition, the control unit 10 includes a first shape control unit 400 and a second shape control unit 500, and receives an input for the aircraft shape from the operator through the control unit 10 (see step S100), or aircraft shape Bring up the control database for the control (see step S200), control the power and signal for the aircraft equipment as described above through the first shape control unit 400, the aircraft equipment through the second shape control unit 500 It is possible to detect whether the equipment is attached or removed.

FIG. 2 is a diagram schematically illustrating a configuration of controlling power and communication signals between equipments of an aircraft multi-shape support experimental system according to an embodiment of the present invention, and the schematic conceptual diagram of FIG. 1 is configured in more detail.

As shown in FIG. 2, the power control unit 200 and the signal control unit 300 may be constituted by a mechanical or electronic relay, and the power control unit 200 and the signal control unit 300 may be connected to the first shape control unit 400. Controlled by the power supply to the aircraft equipment, or to cut off the signal transmitted between each device is implemented through a relay circuit or the like.

3 is a diagram illustrating a mutual relationship in which the second shape control unit 500 included in the control unit 10 senses aircraft equipment according to an embodiment of the present invention.

As shown in FIG. 3, the control unit 10 includes a first shape control unit 400 and a second shape control unit 500, and the second shape control unit 500 is provided by aircraft equipment and cables and other connecting means. It is connected to detect whether the aircraft equipment is mounted / removed.

In this case, the detection of whether the aircraft equipment is mounted or detached is detected through a ground recognition that determines whether the signal connected to the aircraft equipment is grounded by the connection means.

The controller 10 may compare the mounted / detached aircraft equipment identified through the ground recognition with the shape control database read by the operator to determine whether the configuration is consistent with the equipment of the aircraft shape intended by the operator. It is configured to alert the operator if there is a mismatch. Therefore, in many aircraft equipment, it is possible to easily determine whether the equipment constituting the aircraft shape intended by the operator is missing.

4 is a diagram illustrating a method of controlling an experimental system for supporting an aircraft multi-shape according to an embodiment of the present invention.

As shown in FIG. 4, in the method for controlling an aircraft multi-shape support experimental system, the control unit 10 receives an aircraft shape to be implemented in an integrated laboratory (step S100), and the control unit 10 inputs the above. Reading a control database for the received aircraft shape (step S200), detecting whether the second shape control unit 500 is mounted or detached from the aircraft equipment (step S300), and the control unit 10 Comparing the control database and the configuration of the aircraft equipment detected in the step, and if not matched to inform the operator (step S400) and the power control unit 200 and the signal control unit in the first shape control unit 400 And controlling the 300 to form an input aircraft shape (step S500). At this time, the method for detecting the configuration of the aircraft equipment is the second shape control unit 500 when connected to the aircraft equipment to recognize the ground (Ground) through the aircraft equipment to detect the mounting and detachment of the aircraft equipment. Characterized in that.

The step of receiving the aircraft shape in the above may be input selection by the project (basically a variety of purposes, aircraft, naval aircraft, mandatory evacuation aircraft, etc.), or depending on the development version and purchaser.

In addition, through the control database read from the control unit 10, by comparing the aircraft equipment currently connected to the integrated experimental system and the equipment of the input aircraft shape, it is possible to determine whether the equipment of the input aircraft shape is correctly equipped In addition, the operator can easily determine whether the aircraft equipment is connected among a number of aircraft equipment, and can control the communication of power and signals between the equipment for each aircraft using the first shape control unit 400. Will be.

This control method can effectively implement an integrated laboratory that supports a variety of aircraft, and reduce the cost and time required to develop and manufacture an integrated laboratory that supports a single aircraft. In addition, it is possible to automatically recognize the aircraft equipment to prevent the missing part of a number of aircraft equipment in advance, and to control the signal and power between each other aircraft equipment to obtain excellent effect in terms of scalability. Will be.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the disclosed embodiments, but, on the contrary, Those skilled in the art will appreciate that various modifications and changes may be made thereto without departing from the scope of the present invention.

Therefore, the matters of the present invention should not be limited to the embodiments described above, and all of the equivalents or equivalents of the claims, as well as the claims described below, fall within the scope of the spirit of the present invention. I will say.

10:
100: power supply unit 200: power supply control unit
300: signal control unit 400: first shape control unit
500: second shape control unit
S100: step of receiving aircraft shape
S200: reading the aircraft shape control database
S300: Step of detecting whether the aircraft equipment is mounted / detached
S400: Step of determining whether or not the equipment for aircraft by shape
S500: step of controlling the power and communication of the aircraft equipment

Claims (7)

In the aircraft support integrated laboratory equipment used in the aircraft support integrated laboratory,
A control unit 10 for receiving an aircraft shape to be implemented among a plurality of aircraft shapes in the integrated laboratory, and reading a control database for the received aircraft shape and comparing the configurations of a plurality of aircraft equipment mounted in the integrated laboratory. );
A power supply unit 100 supplying power to the mounted plurality of aircraft equipment;
A power control unit 200 controlling power supplied from the power supply unit 100 to the mounted plurality of aircraft equipment;
A signal controller 300 for controlling data signals transmitted and received between the mounted plurality of aircraft equipment;
A first shape control unit 400 controlling the power control unit 200 and the signal control unit 300 according to whether or not the mounted plurality of aircraft equipment is matched with the aircraft shape to be implemented; And
A second shape control unit 500 for detecting whether the aircraft equipment is mounted or detached;
Integrated experimental equipment for supporting aircraft multi-shape comprising.
The method of claim 1,
The power control unit 200 and the signal control unit 300 is integrated experimental equipment for supporting aircraft multi-shape, characterized in that consisting of a mechanical or electronic relay circuit.
delete The method of claim 1,
When the second shape control unit 500 is connected to the aircraft equipment, the integrated experimental equipment for supporting the aircraft multi-shape, characterized in that whether to detect the mounting / detachment of the aircraft equipment through the ground recognition through the aircraft equipment. .
(a) receiving, by the controller 10, an aircraft shape to be implemented among a plurality of aircraft shapes in an integrated laboratory;
(b) reading, by the controller 10, a control database for the aircraft shape input in the step (a);
(c) detecting, by the second shape control unit, whether or not the plurality of aircraft equipment is mounted on or in the integrated laboratory;
(d) comparing, by the controller 10, the configuration of the read control database with the sensed configuration of the aircraft equipment, and notifying the operator if there is a mismatch; And
(e) a power control unit for controlling the power supplied to the plurality of aircraft equipment from the power supply unit 100 for supplying power to the plurality of aircraft equipment mounted in the integrated laboratory; Constructing an aircraft shape to be implemented by controlling a signal control unit 300 for controlling a data signal transmitted and received between each of the plurality of aircraft equipments;
Method for controlling the integrated experimental equipment for supporting aircraft multi-shape comprising.
delete The method of claim 5, wherein
The step (c)
When the second shape control unit 500 is connected to the aircraft equipment, the multi-shape support integrated, characterized in that whether to detect the mounting / detachment of the plurality of aircraft equipment through the ground recognition through the aircraft equipment. How to control the lab equipment.

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