CN104637348A - Portable emergency controlling system and emergency controlling method thereof - Google Patents
Portable emergency controlling system and emergency controlling method thereof Download PDFInfo
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- CN104637348A CN104637348A CN201410806932.5A CN201410806932A CN104637348A CN 104637348 A CN104637348 A CN 104637348A CN 201410806932 A CN201410806932 A CN 201410806932A CN 104637348 A CN104637348 A CN 104637348A
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
Abstract
The invention discloses a portable emergency controlling system and an emergency controlling method thereof. The system is used in an environment without a fixed controlling center to control an aircraft. In the system, a multiprotocol switch is adopted and is connected with the fixed controlling center and a communication server; the communication server is connected with an ADS-B (Automatic Dependent Surveillance-Broadcast) and GPS (Global Position System) receiving unit and a satellite communication unit and is connected with the fixed controlling center through an optical fiber; the communication server transmits information from the multiprotocol switch, the ADS-B and GPS receiving unit, the satellite communication unit and the fixed controlling center to a processing terminal; the processing terminal processes the received data to obtain a flight real-time dynamic state, and commands and controls through an antiaircraft control radio station according to the flight real-time dynamics; the antiaircraft control radio station and the aircraft commands and controls in a form of voice communication, meanwhile, conversation voice data transmitted to the antiaircraft control radio station are input to a processing terminal through an audio input wire, and the processing terminal stores the conversation voice data.
Description
Technical field
The invention belongs to blank pipe technical field.
Background technology
China's air traffic control system focusing the consruction on since " eight or five ", fixed control system at different levels begins to take shape.Meanwhile, portable emergency control system is still the relative weak link in domestic blank pipe field, and portable emergency control system have mobile quick, be easy to the features such as deployment, have irreplaceable effect when holding occasion or accident occurring, therefore portable emergency control system becomes the emphasis of development in recent years.
Portable emergency control system, as can rapid-action miniaturization dry pipe pharmacotherapy, possessing stronger maneuverability, in daily control is on duty, by being connected with fixed Control Centre system or vehicular Control Centre system, realizing the expansion at control seat; Under emergency condition, the feature that portable emergency control system has " little, fast, clever ", harsh conditions can met, as transport routes are obstructed, when vehicular Control Centre system cannot be passed through, enter appointed place in the mode of personnel's portable, complete the emergent blank pipe support mission of the very first time.The dirigibility of control can be strengthened to a great extent, supplement existing Control Centre ability.
Summary of the invention
In view of this, the invention provides a kind of portable emergency control system, be that one can rapid-action miniaturization air traffic control system, compared to fixed Control Centre, possess stronger maneuverability, less volume and weight, be convenient to carry out rapid deployment.
In order to achieve the above object, technical scheme of the present invention is: a kind of portable emergency control system, and for carrying out control and commander to aircraft, this system comprises: control commander unit, ADS-B and GPS receiving element, satellite communication unit and power supply unit.
When this emergent control system is in fixed deployable state, namely when it is in fixed Control Centre, control commander unit is directly connected with fixed Control Centre, receives the radar surveillance data that fixed Control Centre provides, carries out control and commander to aircraft.
When this emergent control system is in mobile deployable state: control commander unit connects ADS-B and GPS receiving element, satellite communication unit, the ADS-B position signalling of aircraft obtained by ADS-B and GPS receiving element and navigation signal, and receive by satellite communication unit the radar surveillance data that fixed Control Centre forwarded by satellite.
Power supply unit is used for powering to other unit in this emergent control system.
Wherein there is in ADS-B and GPS receiving element ADS-B and the GPS receiving equipment of ADS-B antenna and gps antenna and correspondence.
There is in satellite communication unit satellite earth antenna and upper integrated satellite receiving equipment thereof.
Control commanded unit and ADS-B and GPS receiving equipment jointly to case formation first carrying kit, in the first carrying kit, ADS-B and GPS receiving equipment is connected to control commander unit.
By ADS-B antenna, gps antenna and satellite communication unit vanning formation second carrying kit.
Power supply unit vanning is formed power supply box.
Wherein the first carrying kit have ADS-B antenna access port, gps antenna access port, Satellite communication access mouth, fixed Control Centre access port and plant-grid connection mouth; Wherein inner at the first carrying kit, ADS-B antenna access port connects ADS-B receiving equipment, gps antenna access port connects GPS receiving equipment, fixed Control Centre access port is connected to control commander unit, and plant-grid connection mouth is connected to the feeder ear of ADS-B and GPS receiving equipment, GPS receiving equipment and control commander unit.
Power supply box has power supply exit.
ADS-B antenna access port is connected to ADS-B antenna, and gps antenna access port is connected to gps antenna, and Satellite communication access mouth is connected to satellite communication unit; Fixed Control Centre access port is connected and fixed formula Control Centre; Plant-grid connection mouth is connected to power supply exit.
Further, control commander unit comprises the Multi-protocol converter, the communication server, processing terminal and the ground to air command radio set that are connected in turn;
Multi-protocol converter is used for being connected and fixed formula Control Centre, carries out protocol conversion, and be supplied to processing terminal by the communication server to the wired radar monitoring data that fixed Control Centre provides;
The communication server for connecting ADS-B and GPS receiving element and satellite communication unit, and passes through the fixed Control Centre of Fiber connection; The communication server possesses two aspect functions: the state of flight signal receiving the network format that Multi-protocol converter, ADS-B and GPS receiving element and satellite communication unit are sent on the one hand, and unification is supplied to processing terminal; When on the other hand receiving by optical fiber the radar surveillance data that fixed Control Centre sends, convert these radar surveillance data to network format, be supplied to processing terminal;
After processing terminal receives the radar surveillance data of network format, these radar surveillance data are corrected and coordinate transform, and display forms flight path further, thus obtain flight in real time dynamically; After processing terminal receives the state of flight signal of network format, analyze and obtain flight in real time dynamically; Above-mentioned flight dynamically shows by processing terminal in real time;
Operator's console is dynamic by carrying out voice command & control between ground to air command radio set and aircraft in real time according to above-mentioned flight, the conversational speech data that ground to air command radio set sends simultaneously enter processing terminal by audio frequency input line, and processing terminal is preserved these conversational speech data;
ADS-B and GPS receiving equipment is ground receiver; Wherein gps antenna and ADS-B receiving antenna are all connected on ground receiver;
ADS-B antenna receives the ADS-B position signalling that aircraft sends, and is sent to ground receiver;
Gps antenna receives the navigation signal that Navsat sends, and is sent to ground receiver;
After ground receiver receives ADS-B position signalling and navigation signal, after converting thereof into network format, be sent to the communication server as state of flight signal;
Satellite receiving equipment is the low noise amplifier and modulator-demodular unit that connect in turn, and modulator-demodular unit connects the communication server;
Satellite antenna receives the radar surveillance data that fixed Control Centre is forwarded by satellite, after low noise amplifier filtering, converting to can the digital signal of modulated demodulator processes, is converted to the radar surveillance data of network format subsequently, be sent to the communication server by modulator-demodular unit;
Power supply unit adopts gasoline engine generator to be that in system, other unit are powered.
Further, also comprise maritime satellite telephone, fixed Control Centre utilizes maritime satellite telephone and other fixed Control Centre to link up.
Further, fixed Control Centre access port comprises E1 interface and serial ports; Wherein E1 interface passes through Fiber connection in the first carrying kit inside with the communication server, outside by Fiber connection extremely fixed Control Centre at the first carrying kit; Serial ports is connected with Multi-protocol converter in the first carrying kit inside, is connected to fixed Control Centre in the first carrying kit outside.
Further, also comprise lightning protection component in ADS-B and GPS receiving element, lightning protection component sets up around gps antenna, ADS-B receiving antenna and ground receiver.
The present invention provides a kind of emergent method of control of portable emergency control system simultaneously for said system, it is characterized in that, the method is as follows:
When this emergent control system is in fixed deployable state, namely this Account Dept is deployed on fixed Control Centre, then wired radar monitoring data is sent to Multi-protocol converter by fixed Control Centre, wired radar monitoring data is converted to network format through Multi-protocol converter, then processing terminal is transferred to by the communication server, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
When this system is in field movable deployable state, the flight being obtained aircraft by three kinds of modes is dynamic in real time:
(1), wired radar monitoring data is forwarded by satellite by fixed Control Centre, satellite earth antenna receives this radar surveillance data forwarded by satellite, after low noise amplifier filtering, converting to can the digital signal of modulated demodulator processes, converted to the radar surveillance data of network format subsequently by modulator-demodular unit, be sent to the communication server, then processing terminal is transferred to by the communication server, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
(2), ADS-B antenna receives the ADS-B position signalling that aircraft sends, be sent to ground receiver, gps antenna receives the navigation signal that Navsat sends, be sent to ground receiver, after ground receiver receives ADS-B position signalling and navigation signal, after converting thereof into network format, be sent to the communication server as state of flight signal; After processing terminal receives the state of flight signal of network format, analyze and obtain flight in real time dynamically; Processing terminal carries out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
(3), the radar surveillance data of fixed Control Centre are converted to E1 fiber-optic signal, this E1 fiber-optic signal is transmitted through the fiber to the communication server, the communication server converts these radar surveillance data to network format, be supplied to processing terminal, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
Beneficial effect:
1, the present invention is the operation architecture framework that a kind of " fixed-vehicular-portable " is operational mode, this is a kind of open architecture design, Specification is followed in design and development process, the data communication format of use standard and communication process agreement, and compatible existing communication resource interface and the interface of underlying communication network transformation later; Adopt open architecture design simultaneously, the IO interface of multiple opening is provided; And native system adopts modular design, according to actual motion environment, select disparate modules to carry out combination configuration, complete the blank pipe support mission of diversification; Device hardware selected in native system is through strict test and a large amount of matured product used, and using can the device element of continuous firing in the presence of a harsh environment, improves survivability and the adaptive capacity to environment of system.
2, the present invention adopts Miniaturization Design, wherein used equipment is mini-plant, this considerably reduce the volume and weight of whole system, therefore by portable, bear, tow or the portable means such as miniature cross-country vehicle transport, motor-driven in field environment, independent erection, form control command ability, under emergency condition, during as held occasion or accident occurring, portable emergency control equipment has " little, hurry up, spirit " feature, harsh conditions can met, as transport routes are obstructed, when vehicular Control Centre system cannot be passed through, appointed place is entered in the mode of personnel's portable, complete the emergent blank pipe support mission of the very first time.The dirigibility of control can be strengthened to a great extent, supplement existing Control Centre ability.
Accompanying drawing explanation
Fig. 1 is native system Organization Chart;
Fig. 2 is control commander unit composition diagram;
Fig. 3 is ADS-B receiving element composition diagram;
Fig. 4 is that native system is operated in connection under fixed mode and signal flow;
Fig. 5 is that native system is operated in connection under mobile deployment mode and signal flow;
Fig. 6 is connection under the mobile deployment mode of native system when being operated in E1 signal and signal flow;
Fig. 7 is the communication panel design drawing in native system first carrying kit.
Embodiment
To develop simultaneously embodiment below in conjunction with accompanying drawing, describe the present invention.
Embodiment 1,
This system comprises: control commander unit, ADS-B and GPS receiving element, satellite communication unit and power supply unit.
When this emergent control system is in fixed deployable state, namely when it is in fixed Control Centre, control commander unit is directly connected with fixed Control Centre, receives the radar surveillance data that fixed Control Centre provides, carries out control and commander to aircraft.
When this emergent control system is in mobile deployable state: control commander unit connects ADS-B and GPS receiving element, satellite communication unit, the ADS-B position signalling of aircraft obtained by ADS-B and GPS receiving element and navigation signal, and receive by satellite communication unit the radar surveillance data that fixed Control Centre forwarded by satellite.
Power supply unit is used for powering to other unit in this emergent control system.
Wherein there is in ADS-B and GPS receiving element ADS-B and the GPS receiving equipment of ADS-B antenna and gps antenna and correspondence.
There is in satellite communication unit satellite earth antenna and upper integrated satellite receiving equipment thereof.
Control is commanded unit, formation first carrying kit cased jointly by ADS-B and GPS receiving equipment, in the first carrying kit, ADS-B and GPS receiving equipment is connected to control commander unit.
By ADS-B antenna, gps antenna and satellite communication unit vanning formation second carrying kit;
Power supply unit vanning is formed power supply box.
Wherein the first carrying kit have ADS-B antenna access port, gps antenna access port, Satellite communication access mouth, fixed Control Centre access port and plant-grid connection mouth; Wherein inner at the first carrying kit, ADS-B antenna access port connects ADS-B receiving equipment, gps antenna access port connects GPS receiving equipment, fixed Control Centre access port is connected to control commander unit, and plant-grid connection mouth is connected to the feeder ear of ADS-B and GPS receiving equipment, GPS receiving equipment and control commander unit.
Second carrying kit is built with ADS-B antenna, gps antenna and satellite communication unit; Second carrying kit only uses in the shipment of this system, in the deployment of system, directly ADS-B antenna, gps antenna and satellite antenna is taken out from this second carrying kit and can use.
Power supply box has power supply exit.
ADS-B antenna access port is connected to ADS-B antenna, and gps antenna access port is connected to gps antenna, and Satellite communication access mouth is connected to satellite antenna; Fixed Control Centre access port is connected and fixed formula Control Centre; Plant-grid connection mouth is connected to power supply exit.
Embodiment 2,
A kind of portable emergency control system provided by the present invention commands unit, ADS-B and GPS receiving element, satellite communication unit and power supply unit to form primarily of control.System architecture as shown in Figure 1.
Portable emergency control system commands unit, ADS-B and GPS receiving element, satellite communication unit and power supply unit to form by control.
Control commander unit is system core unit, and the signal access of all the other each unit wherein, realizes control function; This unit comprises the Multi-protocol converter, the communication server, processing terminal and the ground to air command radio set that are connected in turn, completes flight dynamic monitoring, to functions such as sky commander, data management, local flight planning management and record replayings.Control commander unit composition as shown in Figure 2.
Multi-protocol converter is connected with fixed Control Centre, is converted to network format, and is supplied to processing terminal by the communication server for the wired radar monitoring data fixed Control Centre provided.When portable system is deployed in fixed Control Centre, during expansion as control seat, Multi-protocol converter can process the wired radar monitoring data that Subscriber Unit provides, and the data processed are sent to the communication server, finally radar surveillance data is supplied to processing terminal.
The communication server connects ADS-B and GPS receiving element and satellite communication unit, and by the fixed Control Centre of Fiber connection; The communication server possesses two aspect functions: the signal receiving the network format that Multi-protocol converter, ADS-B and GPS receiving element and satellite communication unit are sent on the one hand, and unification is supplied to processing terminal; When on the other hand receiving by optical fiber the radar surveillance data that fixed Control Centre sends, convert these radar surveillance data to network format, be supplied to processing terminal.
After processing terminal receives the radar surveillance data of network format, these radar surveillance data are corrected and coordinate transform, and display forms flight path further, thus obtain flight in real time dynamically; After processing terminal receives the state of flight signal of network format, analyze and obtain flight in real time dynamically; Processing terminal carries out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
Simultaneously in the present embodiment, processing terminal allows validated user to manage following data: airport, guidance station, terrestrial reference, Control Centre at different levels of civil aviaton scope, course line, air route, training course line, spatial domain.Allow user to safeguard the relevant field of blank pipe basic data as required, or inquire about specific basic data according to search condition.
The manual typing flight planning in this locality, realization associates with system flight path, realizes track estimation, flight path pairing, flight planning condition managing and conformance monitoring etc.
Processing terminal page can complete record terminal demonstration and operation by intercepting system screen picture mode, possesses timi requirement, recurs speed controlling function; Possess the ability of record blank pipe monitoring data simultaneously, and can recur according to the time period selected and broadcasting speed.
Ground to air command radio set is used for adopting the form of voice communication to carry out command & control between aircraft, the conversational speech data that ground to air command radio set sends simultaneously enter processing terminal by audio frequency input line, processing terminal is preserved these conversational speech data, this achieve the record to empty verbiage sound, playing function when simultaneously processing terminal place can provide selecting of voice data.
ADS-B and GPS receiving element is made up of gps antenna, ADS-B receiving antenna and ground receiver; Wherein gps antenna and ADS-B receiving antenna are all connected on ground receiver.As shown in Figure 3.
Wherein ADS-B antenna receives the ADS-B position signalling that aircraft sends, and is sent to ground receiver; Gps antenna receives the navigation signal that Navsat sends, and is sent to ground receiver; After ground receiver receives ADS-B position signalling and navigation signal, after converting thereof into network format, be sent to the communication server as state of flight signal.
ADS-B signal is the signal sent by aircraft, contains the positional information that aircraft is current.
Connect ADS-B signal by drawing, the region that system cannot be able to cover at radar provides regulatory service for aircraft; In radar coverage, also can be used as a kind of important supplement of existing radar surveillance signal.ADS-B technology has the advantages such as monitor message is abundant, updating decision, data precision are high, construction cost is low.
In ADS-B and GPS receiving element, set up lightning protection component around antenna and receiver in the present embodiment simultaneously, play the effect of lightning rod.
Satellite communication unit comprises satellite antenna, low noise amplifier, modulator-demodular unit and maritime satellite telephone.
Radar surveillance data are forwarded by satellite by fixed Control Centre; Satellite antenna receives this radar surveillance data forwarded by satellite, after low noise amplifier filtering, converting to can the digital signal of modulated demodulator processes, is converted to the radar surveillance data of network format subsequently, be sent to the communication server by modulator-demodular unit; Fixed Control Centre utilizes maritime satellite telephone and other fixed Control Centre to link up.
Satellite communication unit in native system, during for disposing, owing to not having the air traffic control radar monitoring data of wire transmission, needs satellite communication unit to receive by the radar surveillance data of satellite transfer in the wild.
In the present embodiment, maritime satellite telephone can select Inmarsat company to be the customized specific satellite cell-phone IsatPhone Pro of its marine satellite network, for linking up with other fixed Control Centre such as subregion or AREA CONTROL CRNTRE.
Power supply unit adopts gasoline engine generator to be that in system, other unit are powered.
Embodiment 3,
For the system schema provided in embodiment 2, because adopted each equipment all can carry out deployment operation in field, and be easy to carry.And the carrying mode that the mode that the present embodiment proposes a kind of employing two carrying kits and a power supply box is cased to said system, this carrying mode is rationally easy-to-use, and convenient field is disposed.
By processing terminal, to controlling, annexation between command set, Multi-protocol converter, the communication server and ground receiver maintenance is constant, vanning formation first carrying kit; By ADS-B receiving antenna, gps antenna and satellite earth antenna vanning formation second carrying kit; Power supply unit vanning is formed power supply box.
Wherein the first carrying kit has communication panel, this communication panel has ADS-B antennal interface, gps antenna interface, E1 interface, 1 network interface as Satellite communication access mouth, 4 serial ports and power interface, specifically can be designed to as shown in Figure 7.
Wherein ADS-B antennal interface and gps antenna interface are drawn by the ground receiver of the first carrying kit inside, are respectively used to connect ADS-B antenna and gps antenna.
E1 interface is drawn, all for being connected to the optical transmitter and receiver of fixed Control Centre by the communication server of the first carrying kit inside.
Network interface as Satellite communication access mouth is drawn by the communication server, is connected to the modulator-demodular unit in satellite communication unit.
4 serial ports are drawn, for being connected with the serial ports of fixed Control Centre by the Multi-protocol converter of the first carrying kit inside.
Power interface is drawn, for being connected to the power supply unit in power supply box by the power supply port of equipment each in the first carrying kit.
Wherein the second carrying kit only uses in the shipment of this system, in deployment, launches as long as antenna is wherein taken out.
In the present embodiment, by 2 carrying kits and 1 Portable power source case bearing system all devices during portable, consider that human body bears ability and gait of march, each carrying kit (containing installed equipment) general assembly (TW) is all no more than 25Kg.Harness distributes as shown in table 1.
Table 1 harness distributes inventory
Embodiment 4,
Present embodiments provide a kind of emergent method of control being applicable to embodiment 2:
When this system is in fixed deployable state, fixed Control Centre is deployed on by this Account Dept, as shown in Figure 4, then wired radar monitoring data is sent to Multi-protocol converter by fixed Control Centre, wired radar monitoring data is converted to network format through Multi-protocol converter, then processing terminal is transferred to by the communication server, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
When this system is in field movable deployable state, as shown in Figure 5 and Figure 6, the flight of aircraft is obtained by three kinds of modes dynamic in real time:
(1), wired radar monitoring data is forwarded by satellite by fixed Control Centre, satellite earth antenna receives this radar surveillance data forwarded by satellite, after low noise amplifier filtering, converting to can the digital signal of modulated demodulator processes, converted to the radar surveillance data of network format subsequently by modulator-demodular unit, be sent to the communication server, then processing terminal is transferred to by the communication server, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
(2), ADS-B antenna receives the ADS-B position signalling that aircraft sends, be sent to ground receiver, gps antenna receives the navigation signal that Navsat sends, be sent to ground receiver, after ground receiver receives ADS-B position signalling and navigation signal, after converting thereof into network format, be sent to the communication server as state of flight signal; After processing terminal receives the state of flight signal of network format, analyze and obtain flight in real time dynamically; Processing terminal carries out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
(3), the radar surveillance data of fixed Control Centre are converted to E1 fiber-optic signal, this E1 fiber-optic signal is transmitted through the fiber to the communication server, the communication server converts these radar surveillance data to network format, be supplied to processing terminal, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
To sum up, these are only preferred embodiment of the present invention, be not intended to limit protection scope of the present invention.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.
Claims (6)
1. a portable emergency control system, for carrying out control and commander to aircraft, is characterized in that, this system comprises: control commander unit, ADS-B and GPS receiving element, satellite communication unit and power supply unit;
When this emergent control system is in fixed deployable state, namely when it is in fixed Control Centre, described control commander unit is directly connected with fixed Control Centre, receives the radar surveillance data that fixed Control Centre provides, carries out control and commander to aircraft;
When this emergent control system is in mobile deployable state: described control commander unit connects ADS-B and GPS receiving element, satellite communication unit, the ADS-B position signalling of aircraft obtained by ADS-B and GPS receiving element and navigation signal, and receive by satellite communication unit the radar surveillance data that described fixed Control Centre forwarded by satellite;
Described power supply unit is used for powering to other unit in this emergent control system;
Wherein there is in ADS-B and GPS receiving element ADS-B and the GPS receiving equipment of ADS-B antenna and gps antenna and correspondence;
There is in satellite communication unit satellite earth antenna and upper integrated satellite receiving equipment thereof;
Described control commander's unit and described ADS-B and GPS receiving equipment are jointly cased formation first carrying kit, in the first carrying kit, ADS-B and GPS receiving equipment is connected to described control commander unit;
By described ADS-B antenna, gps antenna and satellite communication unit vanning formation second carrying kit;
Described power supply unit vanning is formed power supply box;
Wherein the first carrying kit have ADS-B antenna access port, gps antenna access port, Satellite communication access mouth, fixed Control Centre access port and plant-grid connection mouth; Wherein inner at the first carrying kit, ADS-B antenna access port connects ADS-B receiving equipment, gps antenna access port connects GPS receiving equipment, fixed Control Centre access port is connected to control commander unit, and plant-grid connection mouth is connected to the feeder ear of ADS-B and GPS receiving equipment, GPS receiving equipment and control commander unit;
Power supply box has power supply exit;
ADS-B antenna access port is connected to ADS-B antenna, and gps antenna access port is connected to gps antenna, and Satellite communication access mouth is connected to satellite communication unit; Fixed Control Centre access port is connected and fixed formula Control Centre; Plant-grid connection mouth is connected to power supply exit.
2. a kind of portable emergency control system as claimed in claim 1, is characterized in that, described control commander unit comprises the Multi-protocol converter, the communication server, processing terminal and the ground to air command radio set that are connected in turn;
Described Multi-protocol converter is used for being connected and fixed formula Control Centre, carries out protocol conversion, and be supplied to processing terminal by the communication server to the wired radar monitoring data that fixed Control Centre provides;
The described communication server for connecting ADS-B and GPS receiving element and satellite communication unit, and passes through the fixed Control Centre of Fiber connection; The described communication server possesses two aspect functions: the state of flight signal receiving the network format that Multi-protocol converter, ADS-B and GPS receiving element and satellite communication unit are sent on the one hand, and unification is supplied to processing terminal; When on the other hand receiving by optical fiber the radar surveillance data that fixed Control Centre sends, convert these radar surveillance data to network format, be supplied to processing terminal;
After described processing terminal receives the radar surveillance data of network format, these radar surveillance data are corrected and coordinate transform, and display forms flight path further, thus obtain flight in real time dynamically; After described processing terminal receives the state of flight signal of network format, analyze and obtain flight in real time dynamically; Above-mentioned flight dynamically shows by processing terminal in real time;
Operator's console is dynamic by carrying out voice command & control between described ground to air command radio set and aircraft in real time according to above-mentioned flight, the conversational speech data that ground to air command radio set sends simultaneously enter processing terminal by audio frequency input line, and processing terminal is preserved these conversational speech data;
Described ADS-B and GPS receiving equipment is ground receiver; Wherein gps antenna and ADS-B receiving antenna are all connected on ground receiver;
Described ADS-B antenna receives the ADS-B position signalling that aircraft sends, and is sent to ground receiver;
Described gps antenna receives the navigation signal that Navsat sends, and is sent to ground receiver;
After described ground receiver receives described ADS-B position signalling and described navigation signal, after converting thereof into network format, be sent to the communication server as state of flight signal;
Described satellite receiving equipment is the low noise amplifier and modulator-demodular unit that connect in turn, and described modulator-demodular unit connects the communication server;
Described satellite antenna receives the radar surveillance data that fixed Control Centre is forwarded by satellite, after low noise amplifier filtering, converting to can the digital signal of modulated demodulator processes, is converted to the radar surveillance data of network format subsequently, be sent to the communication server by modulator-demodular unit;
Described power supply unit adopts gasoline engine generator to be that in system, other unit are powered.
3. a kind of portable emergency control system as claimed in claim 1, is characterized in that, also comprise maritime satellite telephone, and described fixed Control Centre utilizes described maritime satellite telephone and other fixed Control Centre to link up.
4. a kind of portable emergency control system as claimed in claim 2, is characterized in that, described fixed Control Centre access port comprises E1 interface and serial ports; Wherein E1 interface passes through Fiber connection in the first carrying kit inside with the described communication server, outside by Fiber connection extremely described fixed Control Centre at the first carrying kit; Described serial ports is connected with described Multi-protocol converter in the first carrying kit inside, is connected to fixed Control Centre in the first carrying kit outside.
5. a kind of portable emergency control system as described in claim 1 or 2, is characterized in that, also comprises lightning protection component in described ADS-B and GPS receiving element, and lightning protection component sets up around gps antenna, ADS-B receiving antenna and ground receiver.
6. the emergent method of control of a kind of portable emergency control system as claimed in claim 2, it is characterized in that, the method is as follows:
When this emergent control system is in fixed deployable state, namely this Account Dept is deployed on fixed Control Centre, then wired radar monitoring data is sent to Multi-protocol converter by fixed Control Centre, wired radar monitoring data is converted to network format through Multi-protocol converter, then processing terminal is transferred to by the communication server, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set;
When this system is in field movable deployable state, the flight being obtained aircraft by three kinds of modes is dynamic in real time:
(1), wired radar monitoring data is forwarded by satellite by fixed Control Centre, satellite earth antenna receives this radar surveillance data forwarded by satellite, after low noise amplifier filtering, converting to can the digital signal of modulated demodulator processes, converted to the radar surveillance data of network format subsequently by modulator-demodular unit, be sent to the communication server, then processing terminal is transferred to by the communication server, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set,
(2), ADS-B antenna receives the ADS-B position signalling that aircraft sends, be sent to ground receiver, gps antenna receives the navigation signal that Navsat sends, be sent to ground receiver, after ground receiver receives described ADS-B position signalling and described navigation signal, after converting thereof into network format, be sent to the communication server as state of flight signal; After described processing terminal receives the state of flight signal of network format, analyze and obtain flight in real time dynamically; Processing terminal carries out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set;
(3), the radar surveillance data of fixed Control Centre are converted to E1 fiber-optic signal, this E1 fiber-optic signal is transmitted through the fiber to the communication server, the communication server converts these radar surveillance data to network format, be supplied to processing terminal, processing terminal corrects and coordinate transform these radar surveillance data, and display forms flight path further, thus obtain flight in real time dynamically, and carry out command & control according to above-mentioned flight is dynamic in real time by ground to air command radio set.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410806932.5A CN104637348A (en) | 2014-12-22 | 2014-12-22 | Portable emergency controlling system and emergency controlling method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410806932.5A CN104637348A (en) | 2014-12-22 | 2014-12-22 | Portable emergency controlling system and emergency controlling method thereof |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107179778A (en) * | 2017-06-21 | 2017-09-19 | 四川九洲空管科技有限责任公司 | UAV Flight Control method and device with automatic dependent surveillance function |
| CN109035874A (en) * | 2018-08-27 | 2018-12-18 | 中国电子科技集团公司第二十八研究所 | A kind of flat cluster airspace use monitoring method and system of multi-source |
| CN109728846A (en) * | 2018-12-06 | 2019-05-07 | 芜湖市努尔航空信息科技有限公司 | A kind of data processing method and system of air communications |
| CN111121769A (en) * | 2019-12-30 | 2020-05-08 | 中国人民解放军93209部队 | Mechanical scanning portable cooperative target air monitoring equipment and autonomous north correcting method |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107179778A (en) * | 2017-06-21 | 2017-09-19 | 四川九洲空管科技有限责任公司 | UAV Flight Control method and device with automatic dependent surveillance function |
| CN109035874A (en) * | 2018-08-27 | 2018-12-18 | 中国电子科技集团公司第二十八研究所 | A kind of flat cluster airspace use monitoring method and system of multi-source |
| CN109728846A (en) * | 2018-12-06 | 2019-05-07 | 芜湖市努尔航空信息科技有限公司 | A kind of data processing method and system of air communications |
| CN111121769A (en) * | 2019-12-30 | 2020-05-08 | 中国人民解放军93209部队 | Mechanical scanning portable cooperative target air monitoring equipment and autonomous north correcting method |
| CN111121769B (en) * | 2019-12-30 | 2021-11-16 | 中国人民解放军93209部队 | Mechanical scanning portable cooperative target air monitoring equipment and autonomous north correcting method |
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Application publication date: 20150520 |