CN108791943A - A kind of aircraft cross track the guiding land system and method for warship pattern - Google Patents
A kind of aircraft cross track the guiding land system and method for warship pattern Download PDFInfo
- Publication number
- CN108791943A CN108791943A CN201810746317.8A CN201810746317A CN108791943A CN 108791943 A CN108791943 A CN 108791943A CN 201810746317 A CN201810746317 A CN 201810746317A CN 108791943 A CN108791943 A CN 108791943A
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- China
- Prior art keywords
- aircraft
- warship
- cross track
- pattern
- signal lamp
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
Abstract
The guiding that warship pattern the invention discloses a kind of aircraft cross track lands system and method, including greensignal light, orange-colored signal lamp, red eye and the rangefinder being arranged on ship deck；Greensignal light is arranged in the tail portion of ship deck, orange-colored signal lamp, red eye and rangefinder and greensignal light are set gradually above deck, rangefinder is electrically connected by a controller and red eye, and aircraft landing point is between greensignal light and orange-colored signal lamp.The present invention passes through the flight path on the aircraft landing naval vessel for proposing to be physically easier to perform, and the guiding of the guiding land system of warship pattern by aircraft cross track, reduce the degree-of-difficulty factor of aircraft landing, the muscle power and energy for reducing pilot are paid, reduce psychological pressure and operation difficulty that pilot bears, be conducive to improve flight quality and promote flight safety coefficient.
Description
Technical field
The present invention relates to the technical fields of vector aircraft land, and warship pattern more particularly to a kind of aircraft cross track
Guiding land system and method.
Background technology
The offline mode that existing aircraft lands on naval vessel is landed with the slow drop flight path with 4 ° of sea level angle,
At the uniform velocity underway naval vessel is chased finally to land on the deck on naval vessel.During chasing slow drop, use is saturating with Fresnel
The slow drop land with angle are realized in the guide device of microscope group synthesis, the collimated light beam channel that aircraft is provided along Fresnel lens.
In the above process, since descent is long and flight path is all angle of inclination, flight difficulty is larger, and pilot needs
High concentration energy, pays more muscle power and energy, the psychological pressure born also can bigger, the degree-of-difficulty factor of flight safety compared with
Greatly.
Invention content
The guiding that warship pattern the object of the present invention is to provide a kind of aircraft cross track lands system and method, to solve
The above-mentioned problems of the prior art reduces the degree-of-difficulty factor on aircraft landing naval vessel, promotes flight safety coefficient.
To achieve the above object, the present invention provides following schemes：
The guiding that warship pattern the present invention provides a kind of aircraft cross track lands system, including is arranged in ship deck
On greensignal light, orange-colored signal lamp, red eye and rangefinder；
The tail portion on the deck, the orange-colored signal lamp, the red eye and institute is arranged in the greensignal light
It states rangefinder to be successively set on the deck with the greensignal light, the rangefinder passes through a controller and the red
Signal lamp is electrically connected.
Preferably, further include the projection arrangement being arranged in aircraft, the projection arrangement can be shown on the front window of aircraft
Show the projection line and aircraft flight parameter of current flight path.
Preferably, the projection line of the current flight path is revised route projection line.
Preferably, the projection arrangement replaces with helmet mounted display device.
Preferably, the orange-colored signal lamp is arranged in the middle part on the deck, the red eye and the rangefinder
Front on the deck is set and towards the unobstructed position in rear.
Preferably, the greensignal light and the orange-colored signal lamp are in vertical height spacing 2m-5m.
Preferably, the greensignal light and the orange-colored signal lamp are arranged on the central axes of ship navigation longitudinal direction.
Preferably, aircraft enters the initial position of landing preparation stage at least apart from the ships tail portion 1100m.
Preferably, the cross track of aircraft is 20m-60m relative to the flying height on the deck.
The guiding that warship pattern the present invention also provides a kind of aircraft cross track lands method, and aircraft searches out at the uniform velocity straight
The underway naval vessel of line, after substantially determining direction, aircraft enters the landing preparation stage along cross track, and pilot is in cross track
In adjust course at any time, when greensignal light and orange-colored signal lamp position are when on the projection line of the current flight path of aircraft, then aircraft
It is targeted by the land channel on deck, keeps flying height and flying speed constant, chase and close to naval vessel；
The decline critical point of aircraft is A points, and when aircraft flies to A points, rangefinder monitors that aircraft reaches setting with naval vessel
Distance, controller, which sends out instruction, makes red eye open, after pilot sees that red eye lights, operating aircraft immediately
Disposably decline aircraft altitude by defined rate of descent, make landing aircraft on the deck on naval vessel, and airplane tail is made to hook resistance
Block rope, complete aircraft it is horizontal the land of warship pattern.
The present invention achieves following technique effect compared with the existing technology：
The present invention warship mould by the flight path on the aircraft landing naval vessel for proposing to be physically easier to perform by aircraft cross track
The guiding of the guiding land system of formula, reduces the degree-of-difficulty factor of aircraft landing, and the muscle power and energy for reducing pilot are paid, and are subtracted
The psychological pressure and operation difficulty that small pilot bears are conducive to improve flight quality and promote flight safety coefficient.
Description of the drawings
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment
Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the present invention
Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the structural schematic diagram for the guiding land system that aircraft cross track of the present invention warship pattern；
Fig. 2 is the schematic diagram of aircraft of the present invention front window display data in landing；
Wherein：The naval vessels 1-, the decks 2-, 3- aircrafts, the sea level 4-, 5- greensignal lights, 6- orange-colored signal lamps, 7- red letter
Signal lamp, 8- rangefinders, 9- downward courses, 10- cross tracks, 11- flight parameters, the projection line of the current flight paths of 12-.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art obtained under the premise of not making the creative labor it is all its
His embodiment, shall fall within the protection scope of the present invention.
The guiding that warship pattern the object of the present invention is to provide a kind of aircraft cross track lands system and method, to solve
Problem of the existing technology reduces the degree-of-difficulty factor on aircraft landing naval vessel, promotes flight safety coefficient.
In order to make the foregoing objectives, features and advantages of the present invention clearer and more comprehensible, below in conjunction with the accompanying drawings and specific real
Applying mode, the present invention is described in further detail.
As shown in Figure 1 to Figure 2：The guiding land system that a kind of aircraft cross track warship pattern is present embodiments provided,
Including greensignal light 5, orange-colored signal lamp 6, red eye 7 and rangefinder 8 on 1 deck 2 of naval vessel is arranged.
The tail portion on deck 2 is arranged in greensignal light 5, and orange-colored signal lamp 6, red eye 7 and rangefinder 8 are believed with green
Signal lamp 5 is successively set on deck 2, and rangefinder 8 is electrically connected by a controller and red eye 7, and controller is chosen as list
Piece machine or PLC controller.Wherein, orange-colored signal lamp 6 is arranged at the middle part on deck 2, and red eye 7 and the setting of rangefinder 8 exist
The front on deck 2 and towards the unobstructed position in rear；Greensignal light 5 and orange-colored signal lamp 6 are in vertical height spacing 2m-
5m, two signal lamps can be clearly seen that by making pilot in the air, will not be lifted because of the longitudinal oscillation stern on naval vessel 1 make it is orange
Signal lamp 6 is blocked and not visible.
The landing point of aircraft 3 is between greensignal light 5 and orange-colored signal lamp 6.Wherein, the downward course 9 of aircraft 3 inclines
Rake angle is 4 °.Greensignal light 5 and orange-colored signal lamp 6, which are arranged, to navigate by water on naval vessel 1 on longitudinal central axes so that naval vessel 1
Lateral oscillation and oscillation in the pitch mode have no substantial effect on the indicative function of the longitudinal direction of signal lamp, so each signal in the present embodiment
Lamp need not be mounted on the requirement that its stationarity can be also realized on stable inertia holder.
Further include the projection arrangement being arranged in aircraft 3, projection arrangement can show current flight path on the front window of aircraft 3
Projection line 12, the height flown of aircraft 3 and the flight parameters 11 such as speed, wherein the projection line 12 of current flight path is revised
Route projection line.While pilot sees route projection line and flight parameter 11, sight is not interfered with, moreover it is possible to which observation flies at any time
The scene in machine 3 front and periphery.Wherein, projection arrangement also can be replaced helmet mounted display device, and helmet mounted display device can also be shown
The flight parameters 11 such as height and the speed that the projection line 12 of current flight path, aircraft 3 fly are shown, and forward observation can be arrived green
Chrominance signal lamp 5 and orange-colored signal lamp 6 are fallen in the helmet is shown.
The board a plane 3 land channel of usual naval vessel 1 is not instead of just on the central axes of the navigation of naval vessel 1, is had centainly
Lateral position deviation, therefore when projection arrangement shows projection line 12 of current flight path, need to make one and repair accordingly
Just, pilot is made still only to need to keep making greensignal light 5 and orange-colored signal lamp 6 while falling on route projection line, you can
It calibrates aircraft 3 and lands the alignment of channel direction, contribute to the centering with land channel in 3 descent of aircraft.
Aircraft 3 enters the initial position ships tail portion 1100m that at least distance is at the uniform velocity navigated by water of landing preparation stage.Wherein,
The distance needs that aircraft 3 enters the landing preparation stage are selected according to the type of aircraft 3, and flying speed is faster, into landing
The distance of preparation stage is bigger.
The cross track 10 of aircraft 3 is 20m-60m relative to the flying height on deck 2.3 cross track 10 of aircraft relative to
The flying height needs on deck 2 are selected according to the length on naval vessel 1 and the type of the oscillation in the pitch mode degree and aircraft 3 that accordingly generate
It selects, the amplitude that the oscillation in the pitch mode on naval vessel 1 makes warship stern lift is bigger, and the speed of aircraft 3 is faster, and cross track 10 is relative to deck 2
Flying height it is higher, distance of the aircraft 3 apart from sea level 4 is also higher, conversely, distance of the aircraft 3 apart from sea level 4 is just
It is lower.
The present embodiment additionally provides a kind of guiding land method that aircraft cross track warship pattern, and aircraft 3 searches out even
The underway naval vessel 1 of speed, after substantially determining direction, aircraft 3 enters the landing preparation stage along cross track 10, and pilot is in level
Course is adjusted at any time in flight path 10, when greensignal light 5 and orange-colored signal lamp 6 are all located at the projection line of the current flight path of aircraft 3
When on 12, then aircraft 3 is targeted by the land channel on deck 2, keeps flying height and flying speed constant, chases and close to warship
Ship 1.
The decline critical point of aircraft is A points, and when aircraft flies to A points, rangefinder 8 monitors that aircraft 3 reaches with naval vessel 1 and sets
Fixed distance, controller, which sends out instruction, makes red eye 7 open, and after pilot sees that red eye 7 lights, manipulates immediately
Aircraft 3 disposably declines 3 height of aircraft by defined rate of descent, makes the land of aircraft 3 on the deck 2 on naval vessel 1, and make aircraft 3
Pintle tangles arrester wires, complete aircraft 3 it is horizontal the land of warship pattern.Wherein, the course line on A points to deck 2 is letdown pattern 9.
Aircraft 3 is according to 3 type of aircraft to determine direction, fixed height, constant speed degree in the offline mode of land preparation stage
Horizontal flight mode, the present embodiment 3 cross track 10 of aircraft warship pattern guiding land system data monitoring and draw
It leads down, when completing the arrival decline critical point A of aircraft 3 of horizontal flight preparation stage, one time falling head lands on naval vessel 1,
Relative to the slow drop offline mode of existing Fresnel guide device, controlling element is more succinct, is almost two-dimentional in a plane
The control of movement, rather than the control of three-dimensional motion effectively reduce the degree-of-difficulty factor of the landing of aircraft 3, reduce the body of pilot
Power and energy are paid, and psychological pressure and operation difficulty that pilot bears are reduced, and are conducive to improve flight quality and promoted to fly
Safety coefficient.
Specific case is applied in this specification, and principle and implementation of the present invention are described, above example
Explanation be merely used to help understand the present invention method and its core concept；Meanwhile for those of ordinary skill in the art,
According to the thought of the present invention, there will be changes in the specific implementation manner and application range.In conclusion in this specification
Appearance should not be construed as limiting the invention.
Claims (10)
1. a kind of aircraft cross track the guiding land system of warship pattern, it is characterised in that：Including being arranged on ship deck
Greensignal light, orange-colored signal lamp, red eye and rangefinder；
The tail portion on the deck, the orange-colored signal lamp, the red eye and the survey is arranged in the greensignal light
Distance meter is successively set on the greensignal light on the deck, and the rangefinder passes through a controller and the danger signal
Lamp is electrically connected.
2. aircraft cross track according to claim 1 the guiding land system of warship pattern, it is characterised in that：Further include
The projection arrangement being arranged in aircraft, the projection arrangement can show the projection line of current flight path and be flown on the front window of aircraft
Machine flight parameter.
3. aircraft cross track according to claim 2 the guiding land system of warship pattern, it is characterised in that：It is described to work as
The projection line of preceding flight path is revised route projection line.
4. aircraft cross track according to claim 3 the guiding land system of warship pattern, it is characterised in that：The throwing
Image device replaces with helmet mounted display device.
5. aircraft cross track according to claim 1 the guiding land system of warship pattern, it is characterised in that：The orange
Chrominance signal lamp is arranged the middle part on the deck, the red eye and the rangefinder be arranged the deck front simultaneously
The position unobstructed towards rear.
6. aircraft cross track according to claim 1 the guiding land system of warship pattern, it is characterised in that：It is described green
Chrominance signal lamp and the orange-colored signal lamp are in vertical height spacing 2m-5m.
7. aircraft cross track according to claim 1 the guiding land system of warship pattern, it is characterised in that：It is described green
Chrominance signal lamp and the orange-colored signal lamp are arranged on the central axes of ship navigation longitudinal direction.
8. aircraft cross track according to claim 1 the guiding land system of warship pattern, it is characterised in that：Aircraft into
Enter the initial position for preparation stage of landing at least apart from the ships tail portion 1100m.
9. aircraft cross track according to claim 1 the guiding land system of warship pattern, it is characterised in that：Aircraft
Cross track is 20m-60m relative to the flying height on the deck.
10. the guiding of the guiding land system of warship pattern based on aircraft cross track described in any one of claim 1-9
Land method, it is characterised in that：
Aircraft searches out the underway naval vessel of uniform rectilinear, and after substantially determining direction, aircraft enters landing along cross track and prepares
Stage, pilot adjust course at any time in cross track, when greensignal light and orange-colored signal lamp are all located at the current of aircraft
When on the projection line of flight path, then aircraft is targeted by the land channel on deck, keeps flying height and flying speed constant, chases
And close to naval vessel；
The decline critical point of aircraft is A points, when aircraft flies to A points, rangefinder monitor aircraft and naval vessel reach setting away from
From controller, which sends out instruction, makes red eye open, and after pilot sees that red eye lights, operating aircraft is by rule immediately
Fixed rate of descent disposably declines aircraft altitude, makes landing aircraft on the deck on naval vessel, and airplane tail is made to hook arrester wires,
Complete aircraft it is horizontal the land of warship pattern.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810746317.8A CN108791943B (en) | 2018-07-09 | 2018-07-09 | Landing guiding system and landing guiding method for aircraft horizontal flight path landing mode |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810746317.8A CN108791943B (en) | 2018-07-09 | 2018-07-09 | Landing guiding system and landing guiding method for aircraft horizontal flight path landing mode |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108791943A true CN108791943A (en) | 2018-11-13 |
| CN108791943B CN108791943B (en) | 2020-05-08 |
Family
ID=64075852
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810746317.8A Active CN108791943B (en) | 2018-07-09 | 2018-07-09 | Landing guiding system and landing guiding method for aircraft horizontal flight path landing mode |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108791943B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109896014A (en) * | 2019-03-28 | 2019-06-18 | 大连民族大学 | A kind of fixed-wing unmanned plane roof air-drop indicating means |
| CN111210668A (en) * | 2019-12-30 | 2020-05-29 | 四川函钛科技有限公司 | Landing stage flight trajectory offset correction method based on time sequence QAR parameter |
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| US20110148661A1 (en) * | 2008-07-02 | 2011-06-23 | Shinichi Shikii | Guiding device |
| WO2012023919A1 (en) * | 2010-08-19 | 2012-02-23 | Stauffer Scott P | Improved boundary/edge marker and related system |
| CN102666281A (en) * | 2009-09-30 | 2012-09-12 | Adb有限责任公司 | Lighting unit for lighting airfields |
| CN105539868A (en) * | 2015-12-25 | 2016-05-04 | 中国航空工业集团公司北京航空制造工程研究所 | Deck equipment, on-board equipment and guiding device and method for carrier landing of aircraft |
| CN205366055U (en) * | 2015-12-31 | 2016-07-06 | 歌尔科技有限公司 | Unmanned aerial vehicle control system that rises and falls |
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2018
- 2018-07-09 CN CN201810746317.8A patent/CN108791943B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110148661A1 (en) * | 2008-07-02 | 2011-06-23 | Shinichi Shikii | Guiding device |
| CN102666281A (en) * | 2009-09-30 | 2012-09-12 | Adb有限责任公司 | Lighting unit for lighting airfields |
| WO2012023919A1 (en) * | 2010-08-19 | 2012-02-23 | Stauffer Scott P | Improved boundary/edge marker and related system |
| CN105539868A (en) * | 2015-12-25 | 2016-05-04 | 中国航空工业集团公司北京航空制造工程研究所 | Deck equipment, on-board equipment and guiding device and method for carrier landing of aircraft |
| CN205366055U (en) * | 2015-12-31 | 2016-07-06 | 歌尔科技有限公司 | Unmanned aerial vehicle control system that rises and falls |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109896014A (en) * | 2019-03-28 | 2019-06-18 | 大连民族大学 | A kind of fixed-wing unmanned plane roof air-drop indicating means |
| CN109896014B (en) * | 2019-03-28 | 2022-11-18 | 徐州臣赐网络科技有限公司 | Fixed-wing unmanned aerial vehicle roof airdrop indicating method |
| CN111210668A (en) * | 2019-12-30 | 2020-05-29 | 四川函钛科技有限公司 | Landing stage flight trajectory offset correction method based on time sequence QAR parameter |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108791943B (en) | 2020-05-08 |
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