Wideband navigation decoy, suppression and interference integrated system based on light guide microwave technology

Abstract

The invention discloses a broadband navigation decoy, suppression and interference integrated system based on a light guide microwave technology. The broadband navigation decoy, suppression and interference integrated system comprises a radar detection subsystem, a photoelectric tracking subsystem, a radio monitoring subsystem, an interception interference subsystem, a navigation decoy subsystem and a main control system. The target is effectively intercepted by adopting a mode of combining interception interference and navigation decoy, and the target can be landed to a specified airspace under the condition that the target is in a controllable state, so that secondary damage of the target to the ground can be greatly avoided, and the safety of facilities and personnel in the airspace governed by the system is effectively ensured. According to the invention, radar detection, photoelectric detection and radio detection are combined to improve the target detection and identification precision and speed of the system; the system has the advantages of being long in acting distance, wide in acting target range, high in maneuvering performance and real-time, and can meet the real requirements of target defense of various important and sensitive airspaces.

Description

Technical Field

[0001] The present invention relates to the technical field of anti-aircraft vehicles, and in particular to a wide-band navigation deception, suppression and interference integrated system based on optical microwave technology. Background Art

[0002] The target is an unmanned device or manned aircraft that uses radio flight control signal equipment and self-contained program control devices. With the rapid development of the target, its application in military and civilian fields has greatly expanded the use of the target.

[0003] At present, the means of defense against targets are mainly divided into air defense missile attack, laser damage strike, capture network capture and radio signal interference. The existing navigation deception systems and methods are:

[0004] The patent (CN117741704A) published in 2024, "An unmanned drone detection and deception system", uses an omnidirectional detector to locate the target, then lures the target to land at a designated location and can replace human supervision in some scenarios.

[0005] The patent (CN115755099B) published in 2023, "A distributed navigation deception system and method for anti-interference drone countermeasures", sends instructions through the central control unit to control the aircraft group to evenly distribute and surround the target, and then implements navigation deception on the target.

[0006] The patent (CN113985461B) published in 2021, "A drone detection, deception system and method", receives three navigation signals from Beidou, GPS, and GLONAS, calculates and processes the decoy signal through an algorithm, and then uses a multi-frequency gain antenna to transmit the decoy signal.

[0007] At present, the publicly reported literature on navigation deception, suppression and jamming systems all use single-frequency or multi-frequency technical solutions. However, the types of target aircraft that can be defended by single-frequency or multi-frequency systems are limited. On the contrary, the use of wide-band technical solutions can greatly increase the types of target aircraft that the system can defend. However, there are currently no systems and methods involving wide-band systems and methods, but practical applications urgently need wide-band systems and methods.

[0008] In summary, there is currently no public literature regarding the integrated wide-band navigation deception, suppression and jamming system. Summary of the invention

[0009] In view of the deficiencies in the prior art, the present invention provides a wide-band navigation deception, suppression and interference integrated system based on optical microwave technology.

[0010] To achieve the above purpose, the technical solution adopted by the present invention is as follows:

[0011] The present invention provides a wide-band navigation deception, suppression and interference integrated system based on optical microwave technology, including a radar detection subsystem, an optoelectronic tracking subsystem, a radio monitoring subsystem, an interception and interference subsystem, a navigation deception subsystem and a main control system;

[0012] The radar detection subsystem is used to detect targets in the airspace under the jurisdiction of the system, and complete the collection of target motion parameter information after detecting the target;

[0013] The optoelectronic tracking subsystem is used to identify and track targets within the airspace under the jurisdiction of the system, and transmit real-time images to the main control system;

[0014] The radio monitoring subsystem is used to monitor, receive and analyze the target flight control signal, so as to obtain the target's position information;

[0015] The interception and jamming subsystem is used to generate and send tunable microwave signals to interfere with the target flight control signals and force the target to land;

[0016] The navigation decoy subsystem is used to generate and send navigation decoy satellite signals to make the target land in the designated airspace;

[0017] The main control system is used for processing information collected by the radar detection subsystem, optoelectronic tracking subsystem, radio monitoring subsystem, interception interference subsystem, and navigation deception subsystem in the system and sending control commands.

[0018] Furthermore, the radar detection subsystem uses a phased array radar to detect targets within the jurisdictional airspace.

[0019] Furthermore, the optoelectronic tracking subsystem is composed of a high-definition camera, an infrared thermal imager, a precision servo turntable and a high-precision tracking module.

[0020] Furthermore, the radio monitoring subsystem consists of a high-gain receiving antenna and a host.

[0021] Furthermore, the interception and jamming subsystem is composed of a pulse drive source, a high-energy pulse cluster fiber laser, a photoconductive semiconductor switch and a radiation component;

[0022] The pulse driving source provides a voltage of 3kv to 10kv for the photoconductive semiconductor switch to ensure that the photoconductive semiconductor switch can work normally;

[0023] The pulse driving source provides voltage to the high-energy pulse cluster fiber laser to ensure that the high-energy pulse cluster fiber laser can operate normally;

[0024] The high-energy pulse cluster fiber laser comprises a high-frequency modulation module and an optical power amplification module. The high-energy pulse cluster fiber laser outputs high-energy laser pulses with sub-pulse frequencies continuously tunable from 0.5 GHz to 10 GHz to a photoconductive semiconductor switch;

[0025] The photoconductive semiconductor switch outputs a tunable microwave signal with a frequency of 0.5 GHz to 10 GHz consistent with the incident laser pulse parameters to the radiation component according to the voltage input by the pulse driving source and the laser pulse input by the high-energy pulse cluster fiber laser;

[0026] The radiation component is used to transmit microwave signals to intercept and interfere with targets.

[0027] Furthermore, the high-frequency modulation module includes an electro-optical intensity modulator and its driving circuit, and an arbitrary signal generator;

[0028] The arbitrary signal generator can output a high-frequency electrical signal of arbitrary waveform in the GHz range;

[0029] The input end of the electro-optic intensity modulator is connected to the output end of the previous optical path, the arbitrary signal generator is connected to the input end of the electro-optic intensity modulator driving circuit by a coaxial signal line, and the output end of the electro-optic intensity modulator driving circuit is connected to the RF input end of the electro-optic intensity modulator by a coaxial signal line. The frequency of the arbitrary signal generator is adjusted to achieve continuous tuning of the sub-pulse frequency of the pulse cluster laser from 0.5 GHz to 10 GHz, thereby generating a 0.5 GHz to 10 GHz continuously tunable microwave signal.

[0030] Furthermore, the navigation decoy subsystem is composed of a satellite signal receiving device, a navigation decoy satellite signal generating device and an antenna assembly;

[0031] The satellite signal receiving device is used to receive the target real satellite signal;

[0032] The navigation decoy satellite signal generating device is used to generate a navigation decoy satellite signal according to the received target real satellite signal;

[0033] The antenna assembly is used to send navigation decoy satellite signals to the target.

[0034] Furthermore, the real satellite signals received by the navigation decoy subsystem include GPS signals, GNSS signals, and Beidou signals.

[0035] Furthermore, the wide-band navigation deception, suppression and interference integrated system based on optical microwave technology can be loaded on a mobile platform.

[0036] The present invention also provides a working method of the above-mentioned wide-band navigation deception, suppression and interference integrated system based on optical microwave technology, comprising the following steps:

[0037] S1, the radar detection subsystem detects the target, collects the target motion parameter information and sends the target motion parameter information to the optoelectronic tracking subsystem;

[0038] S2, the precision servo turntable and high-precision tracking module of the optoelectronic tracking subsystem track the target according to the target motion parameter information provided by the radar detection subsystem, and then use the high-definition camera to capture the image of the target in the airspace under the jurisdiction of the system, and match the image of the target in the airspace under the jurisdiction of the system with the aircraft database for features, and cooperate with the infrared thermal imager to complete the target recognition;

[0039] S3. The radio monitoring subsystem monitors, receives and analyzes the flight control signal of the target, thereby obtaining the target's position information; the main control system determines whether the target is within the system's jurisdictional airspace according to the jurisdictional airspace range set by the system and the target's position information. When the target is within the jurisdictional airspace, the verification result is determined to be "true", and the main control system issues a control command to the interception interference subsystem and the navigation deception subsystem to start the interception interference subsystem and the navigation deception subsystem; when the target is not within the jurisdictional airspace, the verification result is determined to be "false", and the main control system determines that the target's position information is a false alarm, and deletes the target from the radar detection subsystem;

[0040] S4. After the interception and jamming subsystem and the navigation deception subsystem receive the control command, the interception and jamming subsystem emits a microwave signal to interfere with the target's flight control. At the same time, the navigation deception subsystem sends the generated navigation deception satellite signal to the target to complete the target disposal.

[0041] Compared with the prior art, the technical effects that the present invention can produce are:

[0042] The invention provides a wide-band navigation deception, suppression and jamming integrated system based on optical microwave technology, which uses a wide-band tunable microwave signal generated based on optical microwave technology to interfere with the flight control signal of the target. It can tune microwave signals of different frequencies according to the jamming requirements, realize wide-band and high-power radio signal jamming, and expand the target range.

[0043] The present invention transmits the target motion parameter information collected by the radar detection subsystem to the optoelectronic tracking subsystem, and then the precision servo turntable and high-precision tracking module of the optoelectronic tracking subsystem track the target according to the target motion parameter information, thereby realizing real-time tracking of the target; then, the image of the target in the airspace under the jurisdiction of the system taken by the high-definition camera is feature matched with the aircraft database, and the target is identified in conjunction with the infrared thermal imager, and the preliminary identification of the target is further completed on the basis of real-time tracking of the target; then, the azimuth information of the target obtained by the radio monitoring subsystem is further compared and identified with the jurisdiction airspace range set by the system, so as to judge whether the detected target is the target of action; the present invention adopts a combination of radar detection, optoelectronic detection and radio detection to improve the accuracy and speed of target detection and identification of the system, and the present application can detect and identify the target in real time and accurately, and reduce the probability of accidental injury to non-targets.

[0044] The present invention adopts a combination of interception interference and navigation deception to achieve effective interception of the target, and can make the target land in a designated airspace when the target is in a controllable state, which can greatly avoid the target from causing secondary damage to the ground and effectively ensure the safety of facilities and personnel in the airspace under the jurisdiction of the system.

[0045] The present invention has the advantages of long effective distance, wide target range, strong maneuverability and real-time performance, and can meet the actual needs of target defense in various important and sensitive airspaces. BRIEF DESCRIPTION OF THE DRAWINGS

[0046] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on the structures shown in these drawings without paying creative work.

[0047] Figure 1 A schematic diagram of a wide-band navigation deception, suppression, and jamming system based on optical microwave technology provided by an embodiment

[0048] Figure 2 A schematic diagram of the working process of a wide-band navigation deception, suppression and interference integrated system based on optical microwave technology provided by an embodiment;

[0049] Figure 3 A schematic diagram of the structure of an interception and jamming subsystem provided by an embodiment;

[0050] Figure 4 A schematic diagram of the working process of the interception jamming subsystem and the navigation deception subsystem provided in one embodiment. DETAILED DESCRIPTION

[0051] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0052] Reference Figure 1 , an embodiment provides a wide-band navigation deception, suppression, and jamming integrated system based on optical microwave technology, including a radar detection subsystem, an optoelectronic tracking subsystem, a radio monitoring subsystem, an interception jamming subsystem, a navigation deception subsystem, and a main control system;

[0053] The radar detection subsystem is used to detect targets in the airspace under the jurisdiction of the system, and complete the collection of target motion parameter information after detecting the target;

[0054] The optoelectronic tracking subsystem is used to identify and track targets within the airspace under the jurisdiction of the system, and transmit real-time images to the main control system;

[0055] The radio monitoring subsystem is used to monitor, receive and analyze the target flight control signal, so as to obtain the target's position information;

[0056] The interception and jamming subsystem is used to generate and send tunable microwave signals to interfere with the target flight control signals and force the target to land;

[0057] The navigation decoy subsystem is used to generate and send navigation decoy satellite signals to make the target land in the designated airspace;

[0058] The main control system is used for processing information collected by the radar detection subsystem, optoelectronic tracking subsystem, radio monitoring subsystem, interception interference subsystem, and navigation deception subsystem in the system and sending control commands.

[0059] The radar detection subsystem uses a phased array radar to detect targets within the jurisdictional airspace.

[0060] The photoelectric tracking subsystem is composed of a high-definition camera, an infrared thermal imager, a precision servo turntable and a high-precision tracking module.

[0061] The radio monitoring subsystem consists of a high-gain receiving antenna and a host.

[0062] Reference Figure 3 , the interception and interference subsystem is composed of a pulse drive source, a high-energy pulse cluster fiber laser, a photoconductive semiconductor switch and a radiation component;

[0063] The pulse driving source provides a voltage of 3kv to 10kv for the photoconductive semiconductor switch to ensure that the photoconductive semiconductor switch can work normally;

[0064] The pulse driving source provides voltage to the high-energy pulse cluster fiber laser to ensure that the high-energy pulse cluster fiber laser can operate normally;

[0065] The high-energy pulse cluster fiber laser comprises a high-frequency modulation module and an optical power amplification module. The high-energy pulse cluster fiber laser outputs high-energy laser pulses with sub-pulse frequencies continuously tunable from 0.5 GHz to 10 GHz to a photoconductive semiconductor switch;

[0066] The photoconductive semiconductor switch outputs a tunable microwave signal with a frequency of 0.5 GHz to 10 GHz consistent with the incident laser pulse parameters to the radiation component according to the voltage input by the pulse driving source and the laser pulse input by the high-energy pulse cluster fiber laser;

[0067] The radiation component is used to transmit microwave signals to intercept and interfere with targets.

[0068] The high-frequency modulation module includes an electro-optical intensity modulator and its driving circuit, and an arbitrary signal generator;

[0069] The arbitrary signal generator can output a high-frequency electrical signal of arbitrary waveform in the GHz range;

[0070] The input end of the electro-optic intensity modulator is connected to the output end of the previous optical path, the arbitrary signal generator is connected to the input end of the electro-optic intensity modulator driving circuit by a coaxial signal line, and the output end of the electro-optic intensity modulator driving circuit is connected to the RF input end of the electro-optic intensity modulator by a coaxial signal line. The frequency of the arbitrary signal generator is adjusted to achieve continuous tuning of the sub-pulse frequency of the pulse cluster laser from 0.5 GHz to 10 GHz, thereby generating a 0.5 GHz to 10 GHz continuously tunable microwave signal.

[0071] The navigation decoy subsystem is composed of a satellite signal receiving device, a navigation decoy satellite signal generating device and an antenna assembly;

[0072] The satellite signal receiving device is used to receive the target real satellite signal;

[0073] The navigation decoy satellite signal generating device is used to generate a navigation decoy satellite signal according to the received target real satellite signal;

[0074] The antenna assembly is used to send navigation decoy satellite signals to the target.

[0075] The real satellite signals received by the navigation deception subsystem include GPS signals, GNSS signals, and Beidou signals.

[0076] The wide-band navigation deception, suppression and interference integrated system based on optical microwave technology can be loaded on a mobile platform.

[0077] Reference Figure 2 One embodiment provides a working method of the above-mentioned wide-band navigation deception, suppression, and interference integrated system based on optical microwave technology, including the following steps:

[0078] S1, the radar detection subsystem detects the target, collects the target motion parameter information and sends the target motion parameter information to the optoelectronic tracking subsystem;

[0079] S2, the precision servo turntable and high-precision tracking module of the optoelectronic tracking subsystem track the target according to the target motion parameter information provided by the radar detection subsystem, and then use the high-definition camera to capture the image of the target in the airspace under the jurisdiction of the system, and match the image of the target in the airspace under the jurisdiction of the system with the aircraft database for features, and cooperate with the infrared thermal imager to complete the target recognition;

[0080] S3. The radio monitoring subsystem monitors, receives and analyzes the flight control signal of the target, thereby obtaining the target's position information; the main control system determines whether the target is within the system's jurisdictional airspace according to the jurisdictional airspace range set by the system and the target's position information. When the target is within the jurisdictional airspace, the verification result is determined to be "true", and the main control system issues a control command to the interception interference subsystem and the navigation deception subsystem to start the interception interference subsystem and the navigation deception subsystem; when the target is not within the jurisdictional airspace, the verification result is determined to be "false", and the main control system determines that the target's position information is a false alarm, and deletes the target from the radar detection subsystem;

[0081] S4. After the interception and jamming subsystem and the navigation deception subsystem receive the control command, the interception and jamming subsystem emits a microwave signal to interfere with the target's flight control. At the same time, the navigation deception subsystem sends the generated navigation deception satellite signal to the target to complete the target disposal.

[0082] Reference Figure 4, wherein the interception interference subsystem transmits a microwave signal to interfere with the flight control of the target, including: the interception interference subsystem transmits a microwave signal to block the flight control signal of the target, so that the target loses control; specifically, the main control system sends a control instruction to the interception interference subsystem according to the frequency of the target flight control signal monitored by the radio monitoring subsystem, and the interception interference subsystem generates and transmits a microwave signal with the same frequency and high power as the target flight control signal, thereby interfering with or blocking the control of the target flight attitude by the target ground control center; the radar detection subsystem collects the target motion parameter information under the action of the interception interference microwave signal to determine the motion state of the target, if the target is in a forced landing state, the main control system determines that the target disposal is completed; if the target is in a hovering state, the main control system sends a control instruction to the navigation decoy subsystem, and the navigation decoy subsystem sends the generated navigation decoy satellite signal to the target to complete the target disposal, specifically including: the satellite signal receiving device of the navigation decoy subsystem receives the real satellite signal of the target, and demodulates the received real satellite signal to obtain the ephemeris data of the target satellite, and determines the signal frequency and code rate of the target satellite; the satellite signal generating device of the navigation decoy subsystem generates a signal according to the target The carrier control word is determined according to the signal frequency of the target satellite, the code control word is determined according to the code rate of the target satellite, and then the navigation decoy satellite signal corresponding to the target satellite is generated according to the carrier control word and the code control word according to the preset standard and format of the real satellite signal; the generated navigation decoy satellite signal is sent to the target by using the antenna assembly; the radar detection subsystem collects the target motion parameter information of the target under the action of the navigation decoy satellite signal, and transmits it to the optoelectronic tracking subsystem, the precision servo turntable and the high-precision tracking module of the optoelectronic tracking subsystem track the target according to the target motion parameter information provided by the radar detection subsystem, and judges whether the target lands in the designated airspace, if the target lands in the designated airspace, it means that the target disposal is completed; if the target does not land in the designated airspace, it means that the target disposal fails, and the main control system sends a control instruction to the interception interference subsystem again, the interception interference subsystem regenerates a microwave signal with the same frequency and high power as the target flight control signal and transmits the microwave signal to the target, and judges the motion state of the target again, if the target is in a forced landing state, it means that the target disposal is completed; if the target is in a hovering state, the navigation decoy subsystem sends the navigation decoy satellite signal to the target again, and the above steps are repeated until the target disposal is completed.

[0083] Matters not covered by the present invention are known technologies.

[0084] The technical features of the above embodiments may be combined arbitrarily. To make the description concise, not all possible combinations of the technical features in the above embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0085] The above-described embodiments only express several implementation methods of the present application, and the descriptions thereof are relatively specific and detailed, but they cannot be understood as limiting the scope of the invention. It should be pointed out that, for a person of ordinary skill in the art, several modifications and improvements can be made without departing from the concept of the present application, and these all belong to the protection scope of the present application. Therefore, the protection scope of the present application shall be subject to the attached claims.

[0086] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. A broadband navigation deception, suppression and jamming system based on optical microwave technology, characterized in that: It includes radar detection subsystem, optoelectronic tracking subsystem, radio monitoring subsystem, interception and jamming subsystem, navigation deception subsystem and main control system; The radar detection subsystem is used to detect targets in the airspace under the jurisdiction of the system, and complete the collection of target motion parameter information after detecting the target; The optoelectronic tracking subsystem is used to identify and track targets within the airspace under the jurisdiction of the system, and transmit real-time images to the main control system; The radio monitoring subsystem is used to monitor, receive and analyze the target flight control signal, so as to obtain the target's position information; The interception and jamming subsystem is used to generate and send tunable microwave signals to interfere with the target flight control signals and force the target to land; The navigation decoy subsystem is used to generate and send navigation decoy satellite signals to make the target land in the designated airspace; The main control system is used for processing information collected by the radar detection subsystem, optoelectronic tracking subsystem, radio monitoring subsystem, interception interference subsystem, and navigation deception subsystem in the system and sending control commands.

2. A wide-band navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 1, characterized in that: The radar detection subsystem uses a phased array radar to detect targets within the jurisdictional airspace.

3. The broadband navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 1, characterized in that: The photoelectric tracking subsystem is composed of a high-definition camera, an infrared thermal imager, a precision servo turntable and a high-precision tracking module.

4. The wide-band navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 1, characterized in that: The radio monitoring subsystem consists of a high-gain receiving antenna and a host.

5. The broadband navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 1, characterized in that: The interception and jamming subsystem is composed of a pulse drive source, a high-energy pulse cluster fiber laser, a photoconductive semiconductor switch and a radiation component; The pulse driving source provides a voltage of 3kv to 10kv for the photoconductive semiconductor switch to ensure that the photoconductive semiconductor switch can work normally; The pulse driving source provides voltage to the high-energy pulse cluster fiber laser to ensure that the high-energy pulse cluster fiber laser can operate normally; The high-energy pulse cluster fiber laser comprises a high-frequency modulation module and an optical power amplification module. The high-energy pulse cluster fiber laser outputs high-energy laser pulses with sub-pulse frequencies continuously tunable from 0.5 GHz to 10 GHz to a photoconductive semiconductor switch; The photoconductive semiconductor switch outputs a tunable microwave signal with a frequency of 0.5 GHz to 10 GHz consistent with the incident laser pulse parameters to the radiation component according to the voltage input by the pulse driving source and the laser pulse input by the high-energy pulse cluster fiber laser; The radiation component is used to transmit microwave signals to intercept and interfere with targets.

6. A broadband navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 5, characterized in that: The high-frequency modulation module includes an electro-optical intensity modulator and its driving circuit, and an arbitrary signal generator; The arbitrary signal generator can output a high-frequency electrical signal of arbitrary waveform in the GHz range; The input end of the electro-optic intensity modulator is connected to the output end of the previous optical path, the arbitrary signal generator is connected to the input end of the electro-optic intensity modulator driving circuit by a coaxial signal line, and the output end of the electro-optic intensity modulator driving circuit is connected to the RF input end of the electro-optic intensity modulator by a coaxial signal line. The frequency of the arbitrary signal generator is adjusted to achieve continuous tuning of the sub-pulse frequency of the pulse cluster laser from 0.5 GHz to 10 GHz, thereby generating a 0.5 GHz to 10 GHz continuously tunable microwave signal.

7. The broadband navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 1, characterized in that: The navigation decoy subsystem is composed of a satellite signal receiving device, a navigation decoy satellite signal generating device and an antenna assembly; The satellite signal receiving device is used to receive the target real satellite signal; The navigation decoy satellite signal generating device is used to generate a navigation decoy satellite signal according to the received target real satellite signal; The antenna assembly is used to send navigation decoy satellite signals to the target.

8. A broadband navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 7, characterized in that: The real satellite signals received by the navigation deception subsystem include GPS signals, GNSS signals, and Beidou signals.

9. The broadband navigation deception, suppression and jamming integrated system based on optical microwave technology as claimed in claim 1, characterized in that: The optical microwave-based wide-band navigation deception, suppression and interference integrated system can be loaded on a mobile platform.

10. The working method of a wide-band navigation deception, suppression and interference integrated system based on optical microwave technology as claimed in claim 1, characterized in that: The following steps are involved: S1, the radar detection subsystem detects the target, collects the target motion parameter information and sends the target motion parameter information to the optoelectronic tracking subsystem; S2, the precision servo turntable and high-precision tracking module of the optoelectronic tracking subsystem track the target according to the target motion parameter information provided by the radar detection subsystem, and then use the high-definition camera to capture the image of the target in the airspace under the jurisdiction of the system, and match the image of the target in the airspace under the jurisdiction of the system with the aircraft database for features, and cooperate with the infrared thermal imager to complete the target recognition; S3, the radio monitoring subsystem monitors, receives and analyzes the flight control signal of the target, thereby obtaining the target's position information; The main control system determines whether the target is within the airspace under the jurisdiction of the system according to the scope of the airspace under the jurisdiction set by the system and the azimuth information of the target. When the target is within the airspace under the jurisdiction, the verification result is determined to be "true", and the main control system sends a control command to the interception jamming subsystem and the navigation deception subsystem to start the interception jamming subsystem and the navigation deception subsystem; When the target is not in the jurisdiction airspace, the verification result is judged to be "false", and the main control system determines that the target's position information is a false alarm, and deletes the target from the radar detection subsystem; S4. After the interception and jamming subsystem and the navigation deception subsystem receive the control command, the interception and jamming subsystem emits a microwave signal to interfere with the target's flight control. At the same time, the navigation deception subsystem sends the generated navigation deception satellite signal to the target to complete the target disposal.

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