An aerial measurement mission system for a light fixed-wing aircraft

Abstract

This invention belongs to the field of aerial surveying technology, and particularly relates to an aerial surveying mission system for a light fixed-wing aircraft. It includes a light fixed-wing aircraft and an aerial surveying mission system mounted on the aircraft. During aerial surveying missions, the light fixed-wing aircraft is equipped with a pilot, navigator, photographer, and operator. After the pilot and crew reach the designated altitude and target area, the operator opens the sliding door of the mechanically opening and closing camera window. The navigator then operates the aircraft to enter the target aerial surveying route, and the photographer operates the aerial camera mounted on the camera window to perform the aerial surveying mission. This invention improves the overall efficiency of aerial surveying missions and provides an aerial surveying mission system for a light fixed-wing aircraft with a large speed and altitude envelope, good adaptability, effectively improved safety, good maintainability and reliability, and high efficiency and economy.

Description

Technical Field

[0001] This invention belongs to the field of aerial surveying technology, and particularly relates to an aerial surveying mission system for a light fixed-wing aircraft. Background Technology

[0002] Aerial surveying is a method of collecting mapping information or other images using aircraft, helicopters, drones, balloons, or other aerial methods. Typical data collected includes aerial photography, lidar, remote sensing (using various visible and invisible electromagnetic spectrum bands, such as infrared, gamma, or ultraviolet), and geophysical data (such as airborne magnetic surveys and gravity). With the needs of my country's economic development and national defense construction, there is an urgent need for a large amount of map data. Therefore, aerial surveying has developed rapidly, and various surveying and mapping departments have successively established aerial surveying agencies to conduct aerial mapping services. The application of large-scale aerial mapping technology has been widely promoted in various surveying and mapping departments.

[0003] US Patent 14565252 proposes an aerial surveying aircraft with a protective hood for an infrared camera lens used in aerial surveying, solving the problems of vibration reduction and camera lens protection for aerial surveying infrared cameras, but not solving the problem of rapid disassembly of aerial cameras; Chinese Patent 201922267987.4 proposes a lidar aerial surveying aircraft, which reduces the probability of the aerial surveying aircraft crashing due to malfunction by adding a parachute device, but due to the weight limit of UAVs, it is not possible to install an aerial surveying mission system capable of performing low-altitude, large-scale aerial surveying missions; Chinese Patent 201922268019.5 proposes an aerial surveying system based on 5G communication, which partially solves the problems of low efficiency in aerial surveying missions and data loss due to signal blockage, but does not solve the problem of electromagnetic compatibility of external antennas. Summary of the Invention

[0004] The purpose of this invention is to upgrade aerial survey aircraft, improve the overall efficiency of aerial survey missions, and provide an aerial survey mission system for a light fixed-wing aircraft with a large speed and altitude envelope, good adaptability, effective improvement of aerial survey mission safety, good maintainability and reliability, and high aerial survey efficiency and economy.

[0005] The technical solution of the present invention:

[0006] An aerial surveying mission system for a light fixed-wing aircraft, the system comprising: a light fixed-wing aircraft and an aerial surveying mission system mounted on the light fixed-wing aircraft;

[0007] When performing aerial surveying missions, the light fixed-wing aircraft is equipped with a pilot, navigator, photographer, and operator. After the pilot drives the light fixed-wing aircraft with the passengers to the designated altitude and target area, the operator opens the sliding door of the mechanically openable photography window 23, the navigator operates the aircraft to enter the target aerial survey route, and the photographer operates the aerial photography camera installed on the photography window 23 to perform the aerial surveying mission.

[0008] Furthermore, the light fixed-wing aircraft is equipped with a mechanically opening and closing photography window 23. This door opens rearward when performing aerial survey missions, and a micro switch is installed at the maximum opening angle. The navigator seat 11, photographer seat 12, and operator seat 13 are bolted to the aircraft's bulkhead rails and floor rails. The seat backs are adjustable, and the seats are equipped with seat belts. The living equipment cabinet 14 is located on the left side of the front of the cabin floor. The living equipment cabinet 14 consists of an equipment cabinet, a kettle, and an oven. The oven is fixed to the upper surface of the equipment cabinet. Vibration reduction measures are taken for the oven's installation. The kettle base is fixed to a tray, and the tray has a water-retaining groove.

[0009] Furthermore, the navigator's control panel 21 is located on the right side of the front of the cabin floor. A navigator's instrument panel 211 is mounted on the control panel. The instrument panel 211 includes a fiber optic inertial navigation system control display showing navigation information to guide the navigator in navigation tasks; an aviation clock displaying flight time and current time; an electronic integrated display showing airspeed and altitude information; a high-precision altitude indicator showing aircraft altitude information; an atmospheric total temperature indicator showing real-time outside air temperature; an electronic horizontal position indicator indicating the aircraft's magnetic heading, true heading, and other radio navigation information; a turn indicator light illuminating when the aircraft turns to provide the navigator with a turn prompt; and a camera sliding door position indicator light providing the navigator with the camera sliding door's position indication. The camera sliding door turns green when it reaches a designated position and triggers a microswitch, and yellow in other states. The navigator communicates with other crew members by inserting a headset microphone into the headset microphone jack and operating the communication control box.

[0010] Furthermore, the photographer's control panel 22 is located on the right side of the rear cabin floor. A photographer's instrument panel 221 is installed on the control panel. The photographer's instrument panel 221 is equipped with an aviation clock to display flight time and current time for the navigator, a ground speed and current deviation indicator to display ground speed and current deviation indication, an airspeed indicator to indicate the aircraft's airspeed, an atmospheric total temperature indicator to display the real-time atmospheric temperature outside the cabin, a barometric altimeter to display the aircraft's altitude information, a turn indicator light to illuminate when the aircraft turns to provide the photographer with a turn prompt, and a camera sliding door position indicator light to provide the photographer with the position indication of the camera sliding door. The indicator light turns green when the camera sliding door opens to the designated position and triggers a microswitch, and yellow in other states. The photographer can communicate with other crew members by inserting the headset microphone into the headset microphone jack and operating the communication control box.

[0011] Furthermore, the light fixed-wing aircraft is externally equipped with various antennas 15 and mechanically opening and closing camera windows 23; the mechanically opening and closing camera windows 23 can protect the lenses of aerial photography cameras.

[0012] The various antennas 15 include: HF antenna a, 1#VHF antenna b, 2#VHF antenna c, two radio altimeter antennas d, upper transponder antenna e, lower transponder antenna f, collision avoidance lower antenna g, collision avoidance upper antenna h, weather radar antenna i, airborne transponder front antenna j, airborne transponder rear antenna k, multimode combined antenna ADFl, multimode beacon antenna m, multimode microwave landing antenna n, multimode ranging antenna o, multimode Vortex / heading / glide slope combined antenna p, satellite receiving antenna q, and 2#GPS antenna r.

[0013] Furthermore, HF antenna a, 1#VHF antenna b, and 2#VHF antenna c belong to the communication system. HF antenna a is obliquely arranged between the aircraft's vertical tail and the rear fuselage, 1#VHF antenna b is installed below the nose, and 2#VHF antenna c is installed above the rear fuselage.

[0014] Furthermore, the two radio altimeter antennas d, the upper transponder antenna e, the lower transponder antenna f, the lower anti-collision antenna g, the upper anti-collision antenna h, the weather radar antenna i, the front antenna of the airborne transponder j, the rear antenna of the airborne transponder k, the multi-mode combined antenna ADFl, the multi-mode beacon antenna m, the multi-mode microwave landing antenna n, the multi-mode ranging antenna o, the multi-mode Volt / heading / glide combination antenna p, and the satellite receiving antenna q belong to the navigation system;

[0015] Two radio altimeter antennas (d) are installed below the aft fuselage; the upper transponder antenna (e) is installed slightly to the left of the upper part of the front of the passenger cabin section in the middle fuselage; the lower transponder antenna (f) is installed slightly to the right of the lower part of the front cockpit section in the forward fuselage; the lower collision avoidance antenna (g) is installed slightly to the left of the lower part of the front cockpit section in the forward fuselage; the upper collision avoidance antenna (h) is installed slightly to the right of the upper part of the junction between the aft and mid-fuselage; the weather radar antenna (i) is installed inside the nose radome; the front transponder antenna (j) is installed slightly to the right of the upper part of the forward baggage compartment; the rear transponder antenna (k) is installed in the middle of the lower part of the junction between the middle and aft fuselages; the multimode combined antenna (ADFl) is installed in the middle of the lower part of the junction between the aft and mid-fuselage; the multimode beacon antenna (m) is installed in the middle of the lower part of the front of the passenger cabin section in the middle fuselage; the multimode microwave landing antenna (n) is installed slightly to the right of the upper part of the nose; the multimode ranging antenna (o) is installed slightly to the right of the lower part of the front center of the passenger cabin section in the middle fuselage; the multimode Vortex / heading / glide slope combined antenna (p) is installed on the vertical stabilizer; and the satellite receiving antenna (q) is installed slightly to the right of the upper part of the junction between the aft and mid-fuselage.

[0016] Furthermore, GPS antenna #2 belongs to the mission system;

[0017] The #2 GPS antenna is installed on the upper right side of the front center section of the mid-fuselage cabin.

[0018] This invention presents an aerial surveying mission system based on a light fixed-wing aircraft, enabling the upgrading of aerial surveying aircraft and significantly improving the overall efficiency of aerial surveying missions. Specific advantages include: the light fixed-wing aircraft involved in this invention has a wide speed and altitude envelope, good adaptability, good maintainability and reliability, resulting in high efficiency and economy for aerial surveying missions, effectively improving mission safety and availability; the invention solves the electromagnetic compatibility problem of dense external antenna arrangements on light fixed-wing aircraft through overall optimization of the external antenna layout; the invention designs a dedicated mechanically opening and closing camera window, which is highly adaptable and enables rapid loading and unloading of aerial cameras, improving aerial surveying efficiency; the navigator's seat, photographer's seat, and operator's seat designed in this invention fully consider ergonomics, providing high comfort and reducing fatigue during aerial surveying missions; the aerial surveying mission system designed in this invention enables the upgrading of aerial surveying aircraft mission equipment, significantly improving its mission capabilities; the living quarters cabinet designed in this invention fully considers the user's needs for in-flight food and water heating, providing backup support for aerial surveying missions and greatly improving comfort. Attached Figure Description

[0019] Figure 1 This is an organizational structure diagram of the airborne surveying mission system;

[0020] Figure 2 This is a schematic diagram of the equipment layout inside the cabin;

[0021] Figure 3 This is a schematic diagram of the external antenna arrangement (for illustration only) and the mechanically opening and closing camera window;

[0022] Figure 4 This is a detailed schematic diagram of the external antenna layout (left view);

[0023] Figure 5 This is a detailed schematic diagram (top view) of the external antenna layout;

[0024] In the diagram: 1-Light fixed-wing aircraft; 2-Dedicated aerial surveying mission system; 11-Navigator's seat; 12-Photographer's seat; 13-Operator's seat; 14-Living equipment cabinet; 15-External antenna (illustrated only); 21-Navigator's console; 22-Photographer's console; 23-Mechanically opening and closing camera window; 211-Navigator's instrument panel; 221-Photographer's instrument panel;

[0025] a-HF antenna, b-1#VHF antenna, c-2#VHF antenna, d-two radio altimeter antennas, e-upper transponder antenna, f-lower transponder antenna, g-lower anti-collision antenna, h-upper anti-collision antenna, i-weather radar antenna, j-front antenna of airborne transponder, k-rear antenna of airborne transponder, l-multimode combined antenna ADF, m-multimode beacon antenna, n-multimode microwave landing antenna, o-multimode ranging antenna, p-multimode Vortex / heading / glide slope combined antenna, q-satellite receiving antenna, r-2#GPS antenna. Detailed Implementation

[0026] The technical solution of the present invention will now be described in detail with reference to the accompanying drawings.

[0027] This invention provides an aerial measurement mission system based on a light fixed-wing aircraft, such as... Figure 1 As shown, the system includes a light fixed-wing aircraft 1 and a dedicated aerial surveying system 2. The light fixed-wing aircraft has external antennas for the relevant aerial surveying equipment mounted on its fuselage, and a mechanically opening and closing camera window. The cabin contains a navigator's seat, a photographer's seat, an operator's seat, and living quarters. The dedicated aerial surveying system includes a navigator's console, a photographer's console, and a mechanically opening and closing camera window.

[0028] When placing antennas on the outside of the aircraft, it is necessary to consider both the aerodynamic shape of the aircraft and the function of the antenna itself to prevent distortion of the antenna's directivity that could affect its normal operation. It is also necessary to consider the mutual isolation between antennas, especially to prevent blocking interference between the transmitting and receiving antennas, power backflow, and radio frequency radiation hazards from high-power antennas.

[0029] A mechanically opening and closing camera window is located on the rear floor of the cabin. It opens rearward during aerial survey missions and is equipped with a microswitch at its maximum opening distance. The mechanically opening and closing camera window consists of a reinforced aircraft frame structure, a camera mounting bracket, a camera window floor, optical glass, a camera sliding door, and a sliding door operating mechanism. The camera mounting bracket is designed with a mechanical interface based on current mainstream aerial photography cameras and mounts (with pre-installed support plates and nuts), allowing for rapid loading, unloading, and conversion between different aerial photography equipment. The navigator's seat, photographer's seat, operator's seat, and living quarters are bolted to the aircraft's bulkhead rails and floor rails.

[0030] The navigator's control panel is located on the right side of the front of the cabin floor. The navigator's instrument panel is installed on the control panel and includes a fiber optic inertial navigation system control display, an aviation clock, an electronic integrated display, a high-precision altitude indicator, an atmospheric total temperature indicator, an electronic level position indicator, a turn indicator, a camera sliding door position indicator, a communication control box, and a headphone / microphone jack.

[0031] The photographer's control panel is located on the right side of the rear cabin floor. The control panel is equipped with a photographer's instrument panel, which includes an aviation clock, ground speed velocities indicator, airspeed indicator, total atmospheric temperature indicator, barometric altimeter, turn indicator, camera sliding door position indicator, aircraft communication control box, and headphone / microphone jack.

[0032] The living equipment cabinet is located on the left side of the front of the cabin floor. It consists of an equipment cabinet, a kettle, and an oven. The oven is fixed to the upper surface of the equipment cabinet. Vibration reduction measures are taken for the installation of the oven. The kettle base is fixed to a tray with a water-blocking groove to prevent water from overflowing.

[0033] Example:

[0034] Reference Figure 1 , Figure 1 This is an organizational diagram of the aerial surveying mission system of the present invention. In this embodiment, the aerial surveying mission system based on a light fixed-wing aircraft includes a light fixed-wing aircraft 1 and a dedicated aerial surveying mission system 2 mounted on the light fixed-wing aircraft. When performing an aerial surveying mission, a pilot, navigator, photographer, and operator are required. After the crew reaches the designated altitude and target area, the operator opens the sliding camera door on the mechanically opening and closing camera window 23. The navigator then operates the aircraft to enter the target aerial surveying route, and the photographer operates the aerial photography camera mounted on the camera window 23 to perform the aerial surveying mission.

[0035] Reference Figure 2 , Figure 2This is a schematic diagram of the equipment layout inside the cabin. The light fixed-wing aircraft is equipped with a mechanically opening and closing camera window 23. This door opens rearward when conducting aerial survey missions, and a microswitch is installed at the maximum opening angle. The navigator seat 11, photographer seat 12, and operator seat 13 are bolted to the aircraft's bulkhead rails and floor rails. The seat backs are adjustable, and the seats are equipped with seat belts. The living equipment cabinet 14 is located on the left side of the front of the cabin floor. The living equipment cabinet 14 consists of an equipment cabinet, a kettle, and an oven. The oven is fixed to the upper surface of the equipment cabinet, and vibration damping measures are taken into account when fixing the oven. The kettle base is fixed to a tray, and the tray has a water-retaining groove to prevent water from overflowing.

[0036] Reference Figure 2 , 3 The navigator's control panel 21 is located on the right side of the front of the cabin floor. A navigator's instrument panel 211 is mounted on the control panel. The instrument panel 211 includes a fiber optic inertial navigation system control display showing navigation information to guide the navigator in navigation tasks; an aviation clock displaying flight time and current time; an electronic integrated display showing airspeed and altitude information; a high-precision altitude indicator showing aircraft altitude information; an atmospheric total temperature indicator showing real-time outside air temperature; an electronic horizontal position indicator indicating the aircraft's magnetic heading, true heading, and other radio navigation information; a turn indicator light illuminating when the aircraft turns to provide the navigator with a turn prompt; and a camera sliding door position indicator light providing the navigator with the camera sliding door's position indication. The indicator light turns green when the camera sliding door opens to the designated position and triggers a microswitch; otherwise, it indicates yellow. The navigator communicates with other crew members by inserting a headset microphone into the headset microphone jack and operating the communication control box. The photographer's console 22 is located on the right side of the rear cabin floor. A photographer's instrument panel 221 is installed on the console. The instrument panel 221 is equipped with an aviation clock to display flight time and current time for the navigator, a ground speed and current deviation indicator to display ground speed and current deviation, an airspeed indicator to indicate the aircraft's airspeed, a total atmospheric temperature indicator to display the real-time atmospheric temperature outside the cabin, a barometric altimeter to display the aircraft's altitude information, a turn indicator light to illuminate when the aircraft turns to provide the photographer with a turn prompt, and a camera sliding door position indicator light to provide the photographer with the position indication of the camera sliding door. The indicator light turns green when the camera sliding door opens to the designated position and triggers a microswitch; otherwise, it turns yellow. The photographer communicates with other crew members by inserting the headset microphone into the headset microphone jack and operating the communication control box.

[0037] Reference Figure 3 , Figure 3This is a schematic diagram of the external antenna arrangement (illustrated only) 15 and the mechanically closable camera window 23. The antenna arrangement shown in the diagram is for illustrative purposes only. The layout should be optimized according to the actual situation of the equipment being carried. When arranging the antennas, it is necessary to consider both the aerodynamic shape of the aircraft and the function of the antennas themselves, to prevent distortions in the antenna's directionality that could affect its normal operation. It is also necessary to consider the mutual isolation between antennas, especially to prevent blocking interference between the transmitting and receiving antennas, power backflow, and radio frequency radiation hazards from high-power antennas. The mechanically closable camera window 23 can protect the lens of the aerial photography camera.

[0038] Reference Figure 4 and Figure 5 The various antennas 15 include: HF antenna a, 1# VHF antenna b, 2# VHF antenna c, two radio altimeter antennas d, upper transponder antenna e, lower transponder antenna f, collision avoidance lower antenna g, collision avoidance upper antenna h, weather radar antenna i, airborne transponder front antenna j, airborne transponder rear antenna k, multimode combined antenna ADFl, multimode beacon antenna m, multimode microwave landing antenna n, multimode ranging antenna o, multimode Vortex / heading / glide combination antenna p, satellite receiving antenna q, and 2# GPS antenna r.

[0039] HF antenna a, VHF antenna b, and VHF antenna c belong to the communication system. HF antenna a is obliquely arranged between the vertical tail and the rear fuselage of the aircraft, VHF antenna b is installed below the nose of the aircraft, and VHF antenna c is installed above the rear fuselage.

[0040] The following antennas belong to the navigation system: two radio altimeter antennas (d), upper transponder antenna (e), lower transponder antenna (f), lower anti-collision antenna (g), upper anti-collision antenna (h), weather radar antenna (i), front antenna of airborne transponder (j), rear antenna of airborne transponder (k), multimode combined antenna (ADFl), multimode beacon antenna (m), multimode microwave landing antenna (n), multimode ranging antenna (o), multimode Volt / heading / glide combination antenna (p), and satellite receiving antenna (q).

[0041] Two radio altimeter antennas (d) are installed below the aft fuselage; the upper transponder antenna (e) is installed slightly to the left of the upper part of the front of the passenger cabin section in the middle fuselage; the lower transponder antenna (f) is installed slightly to the right of the lower part of the front cockpit section in the forward fuselage; the lower collision avoidance antenna (g) is installed slightly to the left of the lower part of the front cockpit section in the forward fuselage; the upper collision avoidance antenna (h) is installed slightly to the right of the upper part of the junction between the aft and mid-fuselage; the weather radar antenna (i) is installed inside the nose radome; the front transponder antenna (j) is installed slightly to the right of the upper part of the forward baggage compartment; the rear transponder antenna (k) is installed in the middle of the lower part of the junction between the middle and aft fuselages; the multimode combined antenna (ADFl) is installed in the middle of the lower part of the junction between the aft and mid-fuselage; the multimode beacon antenna (m) is installed in the middle of the lower part of the front of the passenger cabin section in the middle fuselage; the multimode microwave landing antenna (n) is installed slightly to the right of the upper part of the nose; the multimode ranging antenna (o) is installed slightly to the right of the lower part of the front center of the passenger cabin section in the middle fuselage; the multimode Vortex / heading / glide slope combined antenna (p) is installed on the vertical stabilizer; and the satellite receiving antenna (q) is installed slightly to the right of the upper part of the junction between the aft and mid-fuselage.

[0042] The 2# GPS antenna r belongs to the mission system; the 2# GPS antenna r is installed in the upper right of the front center of the middle fuselage cabin section.

[0043] See Table 1 for detailed information on the installation locations of the external antennas.

[0044] Table 1. Details of External Antennas

[0045]

[0046]

[0047] Compared to existing technologies, the aerial surveying mission system based on a light fixed-wing aircraft designed in this invention represents a significant upgrade to the aerial surveying aircraft, greatly improving the overall efficiency of aerial surveying missions. Specific advantages are as follows:

[0048] 1. The light fixed-wing aircraft involved in this invention has a large speed and altitude envelope, good adaptability, good maintainability and reliability, high efficiency and economy in aerial surveying missions, and can effectively improve the safety and mission attendance rate of aerial surveying missions.

[0049] 2. This invention solves the electromagnetic compatibility problem of dense external antenna arrangement on light fixed-wing aircraft by optimizing the overall layout of the external antenna.

[0050] 3. The invention features a specially designed mechanically opening and closing photographic window, which is highly adaptable and enables rapid loading and unloading of aerial cameras, thereby improving the efficiency of aerial surveying.

[0051] 4. The navigator seat, photographer seat, and operator seat designed in this invention fully consider human-machine interface, provide high comfort, and reduce fatigue during aerial survey missions;

[0052] 5. The aerial survey mission system designed in this invention realizes the upgrading of aerial survey aircraft mission equipment, and its mission capabilities have been greatly improved.

[0053] 6. The living equipment cabinet designed in this invention fully considers the user's needs for heating food and water in the air, providing backup support for aerial survey missions and greatly improving comfort.

Claims

1. An aerial measurement mission system for a light fixed-wing aircraft, characterized in that, The system includes: a light fixed-wing aircraft and an aerial measurement mission system mounted on the light fixed-wing aircraft; When performing aerial surveying tasks, the light fixed-wing aircraft is equipped with a pilot, navigator, photographer and operator. After the pilot drives the light fixed-wing aircraft with passengers to the designated altitude and target area, the operator opens the mechanically openable camera window (23) and the navigator operates the aircraft to enter the target aerial survey route. The photographer operates the aerial photography camera installed on the camera window (23) to perform the aerial surveying task. The light fixed-wing aircraft is equipped with a mechanically openable and closeable photography window (23), and the cabin door opens backward when carrying out aerial survey missions. A micro switch is installed at the maximum opening angle. The light fixed-wing aircraft is equipped with various antennas (15) and mechanically opening and closing photography windows (23) on its exterior; the mechanically opening and closing photography windows (23) protect the lenses of the aerial photography cameras. The various antennas (15) include: HF antenna (a), 1#VHF antenna (b), 2#VHF antenna (c), two radio altimeter antennas (d), upper transponder antenna (e), lower transponder antenna (f), collision avoidance lower antenna (g), collision avoidance upper antenna (h), weather radar antenna (i), airborne transponder front antenna (j), airborne transponder rear antenna (k), multimode combined antenna ADF (l), multimode beacon antenna (m), multimode microwave landing antenna (n), multimode ranging antenna (o), multimode Vortex / heading / glide combination antenna (p), satellite receiving antenna (q), and 2#GPS antenna (r); The HF antenna (a), the #1 VHF antenna (b), and the #2 VHF antenna (c) belong to the communication system. The HF antenna (a) is obliquely arranged between the vertical tail and the rear fuselage of the aircraft, the #1 VHF antenna (b) is installed below the nose of the aircraft, and the #2 VHF antenna (c) is installed above the rear fuselage.

2. The aerial measurement mission system for a light fixed-wing aircraft according to claim 1, characterized in that, The navigator's seat (11), the photographer's seat (12) and the operator's seat (13) are bolted to the aircraft's bulkhead rails and floor rails. The seat backs are adjustable and the seats are equipped with seat belts. The living equipment cabinet (14) is located on the left side of the front of the cabin floor. The living equipment cabinet (14) consists of an equipment cabinet, a kettle and an oven. The oven is fixed to the upper surface of the equipment cabinet. The oven is fixed with vibration reduction measures in mind. The kettle base is fixed to a tray with a water-blocking groove.

3. The aerial measurement mission system for a light fixed-wing aircraft according to claim 1, characterized in that, The navigator's console (21) is located on the right side of the front of the cabin floor. The navigator's instrument panel (211) is installed on the console. The navigator's instrument panel (211) is equipped with a fiber optic inertial navigation system control display that displays navigation information to guide the navigator in performing navigation tasks. The aviation clock displays flight time and current time. The electronic integrated display displays airspeed and altitude information. The high-precision altitude indicator displays the aircraft's altitude information. The total atmospheric temperature indicator displays the real-time atmospheric temperature outside the cabin. The electronic horizontal position indicator indicates the aircraft's magnetic heading and true heading radio navigation information. The turn indicator lights up when the aircraft turns to give the navigator a turn prompt. The camera sliding door position indicator provides the navigator with the position indication of the camera sliding door. It indicates green after the camera sliding door opens to the designated position and triggers the micro switch. The other states indicate yellow. The navigator can communicate with other crew members by inserting the headset microphone into the headset microphone jack and operating the machine communication control box.

4. The aerial measurement mission system for a light fixed-wing aircraft according to claim 1, characterized in that, The photographer's console (22) is located on the right side of the rear cabin floor. The photographer's instrument panel (221) is installed on the console. The photographer's instrument panel (221) is equipped with an aviation clock to display flight time and current time for the navigator, a ground speed and yaw indicator to display ground speed and yaw indication, an airspeed indicator to indicate the aircraft's airspeed, an atmospheric total temperature indicator to display the real-time atmospheric temperature outside the cabin, a barometric altimeter to display the aircraft's altitude information, a turn indicator light to illuminate when the aircraft turns to provide the photographer with a turn prompt, and a camera sliding door position indicator light to provide the photographer with the position indication of the camera sliding door. The camera sliding door is green when it is opened to the designated position and triggers a microswitch, and yellow in other states. The photographer can communicate with other crew members by inserting the headset microphone into the headset microphone jack and operating the machine communication control box.

5. The aerial measurement mission system for a light fixed-wing aircraft according to claim 1, characterized in that, Two radio altimeter antennas (d), upper transponder antenna (e), lower transponder antenna (f), collision avoidance lower antenna (g), collision avoidance upper antenna (h), weather radar antenna (i), airborne transponder front antenna (j), airborne transponder rear antenna (k), multimode combined antenna ADF (l), multimode beacon antenna (m), multimode microwave landing antenna (n), multimode ranging antenna (o), multimode Volt / heading / glide combination antenna (p), and satellite receiving antenna (q) belong to the navigation system; Two radio altimeter antennas (d) are installed below the aft fuselage; the upper transponder antenna (e) is installed slightly to the left of the upper front of the mid-fuselage cabin section; the lower transponder antenna (f) is installed slightly to the right of the lower front of the forward fuselage cockpit section; the lower collision avoidance antenna (g) is installed slightly to the left of the lower front of the forward fuselage cockpit section; the upper collision avoidance antenna (h) is installed slightly to the right of the upper part of the junction between the aft and forward fuselages; the weather radar antenna (i) is installed inside the nose radome; the front transponder antenna (j) is installed slightly to the right of the upper front baggage compartment; and the rear transponder antenna... Antenna (k) is installed in the lower middle of the junction between the mid and aft fuselage; multimode combined antenna ADF (l) is installed in the lower middle of the junction between the front and rear fuselage; multimode beacon antenna (m) is installed in the lower middle of the front of the passenger cabin section of the mid fuselage; multimode microwave landing antenna (n) is installed on the upper right of the nose; multimode ranging antenna (o) is installed on the lower right of the front center of the passenger cabin section of the mid fuselage; multimode Vortex / heading / glide slope combined antenna (p) is installed on the vertical stabilizer; and satellite receiving antenna (q) is installed on the upper right of the junction between the front and rear fuselage.

6. The aerial measurement mission system for a light fixed-wing aircraft according to claim 1, characterized in that, The #2 GPS antenna (r) belongs to the mission system; The 2# GPS antenna (r) is installed on the upper right side of the front center section of the mid-fuselage cabin.

Images