CN110400392A - Flight visual simulation method, apparatus, computer system and readable storage medium storing program for executing - Google Patents
Flight visual simulation method, apparatus, computer system and readable storage medium storing program for executing Download PDFInfo
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Abstract
This application discloses a kind of flight visual simulation methods, vertex of climbing on displacement-altitude curve of flight vertical section for positioning aircraft, flight visual simulation method include: to judge whether displacement-altitude curve includes one Dan Pingfei sections or the flat winged section of multiple ladders；When including Dan Pingfei sections, the starting point of Dan Pingfei sections of positioning is vertex of climbing；In winged section flat including multiple ladders, determine that first flat winged section of ladder for meeting height continuation condition is the flat winged section of cruise starting, height continuation condition refers to that the flat winged section of starting of cruising is higher than predetermined altitude and the duration is greater than the predetermined time；Starting point with the flat winged section of positioning cruise starting is vertex of climbing.In this way, various flight progress can be distinguished and climbed vertex under various flight progress using different strategic orientations, therefore vertex of climbing can be accurately positioned.A kind of flight visual simulation device, computer system and the non-volatile computer readable storage medium storing program for executing comprising computer-readable instruction is also disclosed in the application.
Description
Technical field
This application involves aviation fields, more specifically, are related to a kind of position of flight vertical section of aircraft for identification
The flight visual simulation method on the vertex of climbing (Top of Climb, TOC) on shifting-altitude curve, flight visual simulation device,
Computer system and non-volatile computer readable storage medium storing program for executing comprising computer-readable instruction.
Background technique
Typical flight includes climbing, cruise and declining three phases, is embodied to the position on the flight vertical section of aircraft
Shifting-altitude curve just includes climbing, cruise and declining three straightways.The turning point to climb to cruise is known as the vertex (Top that climbs
Of Climb, TOC), the turning point of cruise to decline is known as declining vertex (Top of Descent, TOD).It is carried out to flight
When technology is analyzed, since the physical features for the three phases that climb, cruise, decline are different, the project and content of analysis are also different, because
This, identifies and positions TOC and TOD is extremely important, it may be said that the largely reasonability and accuracy of influence technique analysis.
Mainly judge TOC in Civil Aviation Industry using empirical method at present, such as artificial visual judgement, height judge, distance is sentenced
It is disconnected.It manually visualizes judgement usually analysis personnel and sees that figure determines TOC based on personal experience.Height judgement can be using computer batch
Amount calculates, and usually gives the height value of an experience, such as 28000 feet (foot, FT) in advance, then aircraft altitude is more than
The flat winged section of first of 28000FT thinks to enter cruising phase.Distance Judgment can also be calculated using computer batch, generally
It is that the last one in the predetermined flying distance of regulation level off a little is TOC, such as the flight time 3 hours or more flights, 300 nautical miles
It is interior the last one level off a little as TOC.
But problem is that the actual displacement of aircraft-altitude curve is not often to climb-is cruised-decline three straightways,
It might have multiple ladders to exist.Current method often can not accurately identify TOC, such as manually visualize judgement and excessively rely on
The experience and professional skill of operator, and general logic cannot be extracted for batch application, to cannot achieve flight skill
The automatic processing of art analysis.
Summary of the invention
The application embodiment provides climbing on a kind of displacement-altitude curve of the flight vertical section of aircraft for identification
The flight visual simulation method of vertex (Top of Climb, TOC) of liter, flight visual simulation device, computer system and comprising
The non-volatile computer readable storage medium storing program for executing of computer-readable instruction.
A kind of flight visual simulation method, climbing on displacement-altitude curve of the flight vertical section for positioning aircraft
Vertex is risen, the flight visual simulation method includes:
Judge whether the displacement-altitude curve includes one Dan Pingfei sections or the flat winged section of multiple ladders；
When including described Dan Pingfei sections, positioning Dan Pingfei sections of the starting point is the vertex of climbing；
When including that multiple ladders equal winged section, first flat winged section of the ladder for meeting height continuation condition is determined
For the flat winged section of cruise starting, the height continuation condition refers to that the flat winged section of the cruise starting is higher than predetermined altitude and the duration is big
In the predetermined time；With
The starting point for positioning the flat winged section of the cruise starting is the vertex of climbing.
A kind of flight visual simulation device, climbing on displacement-altitude curve of the flight vertical section for positioning aircraft
Vertex is risen, the flight visual simulation device includes:
First judgment module, the first judgment module is for judging whether the displacement-altitude curve includes a list
Flat winged section or the flat winged section of multiple ladders；
First locating module, first locating module are used to position when including described Dan Pingfei sections Dan Pingfei sections described
Starting point be the vertex of climbing；
First determining module, first determining module are used to include that multiple ladders determine first when equalling winged section
Meet the flat winged section of the ladder of height continuation condition for the flat winged section of cruise starting, the height continuation condition refers to described cruise
The flat winged section that begins is higher than predetermined altitude and the duration is greater than the predetermined time；With
Second locating module, the starting point that second locating module is used to position the flat winged section of the cruise starting is described
It climbs vertex.
A kind of computer system, the computer system include processor, and the processor is used for:
Judge whether the displacement-altitude curve includes one Dan Pingfei sections or the flat winged section of multiple ladders；
When including described Dan Pingfei sections, positioning Dan Pingfei sections of the starting point is the vertex of climbing；
When including that multiple ladders equal winged section, first flat winged section of the ladder for meeting height continuation condition is determined
For the flat winged section of cruise starting, the height continuation condition refers to that the flat winged section of the cruise starting is higher than predetermined altitude and the duration is big
In the predetermined time；With
The starting point for positioning the flat winged section of the cruise starting is the vertex of climbing.
A kind of computer system, the computer system include:
One or more processors, memory；
One or more programs, wherein one or more of programs are stored in the memory, and described
One or more processors execute, and described program includes for executing the instruction according to the flight visual simulation method.
A kind of non-volatile computer readable storage medium storing program for executing comprising computer-readable instruction, the computer-readable instruction
When being executed by processor, so that the processor executes the flight visual simulation method.
The flight visual simulation method, flight visual simulation device, computer system and include computer-readable instruction
Non-volatile computer readable storage medium storing program for executing can distinguish various flight progress and under various flight progress using different
Strategic orientation TOC, therefore TOC can be accurately positioned under various flight progress.
The additional aspect and advantage of presently filed embodiment will be set forth in part in the description, partially will be from following
Description in become obvious, or recognized by the practice of presently filed embodiment.
Detailed description of the invention
The above-mentioned and/or additional aspect and advantage of the application is from combining in description of the following accompanying drawings to embodiment by change
It obtains obviously and is readily appreciated that, in which:
Fig. 1 is displacement-altitude curve schematic diagram of Typical Aircraft；
Fig. 2-6 is the actual displacement of aircraft-altitude curve schematic diagram；
Fig. 7 is the flow diagram of the flight visual simulation method of one embodiment of the application；
Fig. 8 is the functional block diagram of the flight visual simulation device of one embodiment of the application；
Fig. 9 is the functional block diagram of the computer system of one embodiment of the application；
Figure 10 is another flow diagram of the flight visual simulation method of one embodiment of the application；
Figure 11 is the operation principle schematic diagram of one embodiment of the application；
Figure 12 is the flow diagram of the flight visual simulation method of the application another embodiment；
Figure 13 is the functional block diagram of the computer system of the application another embodiment.
Main element label
Flight visual simulation device 10/10a, first judgment module 12, the first locating module 14, the first determining module 16,
Second locating module 18, the second judgment module 13, the second determining module 15, computer system 100.
Specific embodiment
Presently filed embodiment is described below in detail, the example of the embodiment is shown in the accompanying drawings, wherein identical
Or similar label indicates same or similar element or element with the same or similar functions from beginning to end.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining presently filed embodiment, and should not be understood as to this Shen
The limitation of embodiment please.
It in aviation field, in order to assess the flight reappearance of flight, needs to flight progress technology analysis, such as is tied in flight
Displacement-altitude curve of the flight vertical section of beam post analysis aircraft, so as to evaluate the level that flight executes flight plan,
And then the driving ability of pilot can be evaluated.
It please join Fig. 1, displacement-altitude curve of Typical Aircraft includes climbing, cruise and declining three straightways.It climbs as certainly
The upward skew lines section of takeoff point.Cruise is horizontal linear section.The turning point to climb to cruise is known as vertex (the Top of that climbs
Climb, TOC), that is, it cruises and climbs in TOC connection.Fall to connection cruise and landing point and downward skew lines section.Cruise
Turning point to decline is decline vertex (Top of Descent, TOD), i.e. cruise is connect with decline in TOD.
As an example, the flight that displacement-altitude curve can be recorded by reading the sensor (such as black box) of aircraft
Data obtain flight path, and then calculating available flight path by coordinate transform is including hanging down for takeoff point and landing point
Drop shadow curve on straightforward face, then obtained by data reduction processing (such as smoothed curve).It is appreciated that after treatment
Displacement-altitude curve only includes skew lines section and horizontal linear section.
As background technology part is discussed, when carrying out technology analysis to flight, due to climbing, cruising, declining three
The physical features in stage are different, and the project and content of analysis are also different.Therefore, it identifies and positions TOC and TOD is extremely important, it can
To say the reasonability and accuracy of largely influence technique analysis.
For being typically displaced-altitude curve, due to climbing, to cruising, only one is leveled off a little, and identification TOC is easier,
It can be realized, all can also may be used by computer batch processing (such as height judgement or Distance Judgment) by artificial judgment
Accurately to realize.
However, please join Fig. 2-6, three are cruised-declined to the actual displacement of aircraft-altitude curve is not often to climb-directly
Line segment, and with the presence of multiple ladders, such as climb and will enter cruising phase there may be multiple small ladders, start cruising phase
It is also likely to be present multiple small ladders.Therefore, because have it is multiple level off a little, existing flight visual simulation method is difficult accurately to know
Not.Judge that the figure for complicated line segment depends particularly on the experience and professional skill of operator specifically, manually visualizing, accurately
It spends low, and also results in inefficient.And the height judgement of computer batch processing and Distance Judgment are then due to line segment complexity
It may be cheated, judge by accident, accuracy is equally relatively low by " false TOC ".
Referring to Fig. 7, in view of this, the flight visual simulation method of embodiment of the present invention is used to position the flight of aircraft
Vertex of climbing on displacement-altitude curve of vertical section, flight visual simulation method include:
S12: judge whether displacement-altitude curve includes one Dan Pingfei sections or the flat winged section of multiple ladders；
S14: when including Dan Pingfei sections, the starting point of Dan Pingfei sections of positioning is vertex of climbing；
S16: when including that multiple ladders equal winged section, determine that first flat winged section of ladder for meeting height continuation condition is to patrol
The flat winged section of boat starting, height continuation condition refer to that the flat winged section of cruise starting is higher than predetermined altitude and the duration is greater than the predetermined time；
With
S18: the starting point of the flat winged section of positioning cruise starting is vertex of climbing.
Referring to Fig. 8, the flight that the flight visual simulation device 10 of embodiment of the present invention is used to position aircraft is vertically cutd open
Vertex of climbing on the displacement-altitude curve in face, flight visual simulation device 10 include:
First judgment module 12, first judgment module 12 is for judging whether displacement-altitude curve includes a Dan Pingfei
Section or the flat winged section of multiple ladders；
First locating module 14, the first locating module 14 are used for the starting point of Dan Pingfei sections of the positioning when including Dan Pingfei sections
For vertex of climbing；
First determining module 16, the first determining module 16 are used to include that multiple ladders determine first satisfaction when equalling winged section
The flat winged section of the ladder of height continuation condition is the flat winged section of cruise starting, and it is predetermined that height continuation condition refers to that the flat winged section of cruise starting is higher than
Highly and the duration is greater than the predetermined time；With
Second locating module 18, the starting point that the second locating module 18 is used to position the flat winged section of cruise starting is top of climbing
Point.
It is appreciated that in some embodiments, step S12, S14, S16, S18 can be respectively by first judgment modules
12, the first locating module 14, the first determining module 16, the second locating module 18 execute or implement, and first judges mould in other words
Block 12, the first locating module 14, the first determining module 16, the second locating module 18 may be respectively used for execution or implementation steps
S12,S14,S16,S18.Or say, the flight visual simulation method of embodiment of the present invention can be by embodiment of the present invention
Flight visual simulation device 10 execute or implement.
Certainly, flight processing method can also be not limited to by the realization of flight processing unit 10 or reality in other embodiments
It applies, in other words, Flight Data Unit 10 can also be not limited to be exclusively used in implementing flight visual simulation method.
Certainly, the flight visual simulation method of embodiment of the present invention can also be not limited to be flown by embodiment of the present invention
Row data processing equipment 10 is implemented, and in other words, the flight visual simulation device 10 of embodiment of the present invention can also be not limited to specially
For implementing the flight visual simulation method of embodiment of the present invention.
In some embodiments, first judgment module 12, the first locating module 14, the first determining module 16, second are fixed
Position module 18 can be electronic circuit, such as can be the electronic circuit of discrete component composition, be also possible to integrated circuit,
Wherein, part of module can integrate together, or whole modules are integrated into single IC for both, such as are integrated in as shown in Figure 9
Computer system 100.Computer system 100 may include one or more processors or memory (computer-readable storage
Medium), first judgment module 12, the first locating module 14, the first determining module 16, the second locating module 18 can integrate in one
In a or multiple processors.In other words, processor can be used to implement flight visual simulation method in other words step S12,
S14,S16,S18.In this case, processor can be application specific processor.
In other certain embodiments, first judgment module 12, the first locating module 14, the first determining module 16,
Second locating module 18 can be stored in computer program in memory, computer-readable instruction computer program in other words
Code segment, and can parse, run in the one or more processors 1 of computer system 100, it is one or more at runtime
Processor can be used to implement flight visual simulation method step S12, S14, S16, S18 in other words.In this case, it handles
Device can be general processor, such as can be central processing unit (central processing unit, CPU), processor
It can be the general processor designed and manufactured for certain purpose, such as graphics processor (graphic processing
unit,GPU)。
In some embodiments, computer system 100 can be control centre, airline or airline's control
The a part at center, and pass through the data of the network of airline reading aircraft.Certainly, computer system 100 is also possible to far
Journey, wherein memory can also be remote memory cloud memory in other words.
It is appreciated that exactly step S12, S14, S16, S18 in other words first judgment module 12, the first locating module 14,
First determining module 16, the second locating module 18 are functionally supported each other, interacting just makes flight visual simulation
Method, flight visual simulation device 10, computer system 100 and computer readable storage medium all may be used under various flight progress
TOC is accurately positioned.Specifically, meeting list if flight progress meets typical displacement-altitude curve as shown in Figure 1
The case where flat winged section, can by step S12, S14 in other words first judgment module 12, the first locating module 14 cooperate it is accurate fixed
Position TOC.If the complicated displacement-altitude curve of flight progress as shown in figures 2-6 then can continue item by devising height
The first determining module 16, the second locating module 18 cooperate accurately calmly step S16, S18 of part and reasonable positioning strategy in other words
Position TOC.
It please join Figure 10, step S12 includes:
S122: the horizontal line section on identification displacement-altitude curve is flat winged section；
S124: whether the number of the flat winged section of judgement is 1 or greater than 1；
S126: when the number of flat winged section is 1, determine that displacement-altitude curve includes Dan Pingfei sections；With
S128: when the number of flat winged section is greater than 1, determine that displacement-altitude curve includes the flat winged section of multiple ladders.
Specifically, can judge that the line segment on displacement-altitude curve is by the modes such as image recognition or coordinate calculating
It is no to be horizontal line section or be oblique line section.In this way, flight situation or complicated flight can be distinguished by simply calculating
Situation, to reduce operand.
It please join Figure 11, in some embodiments, height continuation condition includes that a predetermined altitude and one are corresponding pre-
It fixes time.
In these embodiments, can through reasonable settings predetermined altitude and predetermined time find most complete climb
The stage of liter navigates to highest TOC to smooth out the small ladder that will enter cruise in a sense, accordingly it is also possible to
Referred to as " highest scheme TOC ".It is appreciated that although will enter the small ladder height of cruise may meet some requirements, so
And the duration is all shorter.Therefore, in this example, " reasonable that predetermined altitude and predetermined time is arranged " is it may be said that heavier
What is wanted is the setting longer predetermined time, and predetermined altitude can be lowerd instead.For example, in one example, the predetermined time is 10
Minute, predetermined altitude is 10000 feet.Certainly, specific numerical value is not limited to embodiment and can be set according to specific requirements
It sets.
Continuing with ginseng Figure 11, in other embodiment, height continuation condition includes multiple predetermined altitudes and multiple
The corresponding predetermined time.
In these embodiments, can through reasonable settings multiple predetermined altitudes and multiple predetermined times position most
Close to Jeppesen flight plan TOC, compare for doing the practical and plan position TOC, can generally navigate to enter and patrol
It is located in the middle TOC in the small ladder of boat, accordingly it is also possible to be known as " intermediate scheme TOC ".It is appreciated that cruise will be entered
Although small ladder height may meet some requirements, the duration is all shorter.Therefore, in this example, " close
The setting predetermined altitude of reason and the predetermined time " is it may be said that more importantly balance predetermined altitude and matched predetermined time.For example,
In one example, height continuation condition includes three predetermined altitudes and three corresponding predetermined times, for example, predetermined altitude
27000 feet, 2 minutes corresponding predetermined times；20000 feet of predetermined altitude, 5 minutes corresponding predetermined times；Predetermined altitude
10000 feet, 10 minutes corresponding predetermined times.
It is appreciated that specifically can be depending on specific requirements, in fact, in major part using that height continuation condition
Flight progress under, be respectively adopted two kinds of height continuation conditions positioning TOC should be identical.
It please join Figure 12, in some embodiments, flight visual simulation method further include:
S13: judge whether the flat winged section of ladder meets height continuation condition；When meeting height continuation condition, enter step
S14；
S15: when not finding the flat winged section of the ladder for meeting height continuation condition, the determining highest nearest from takeoff point or most
The flat winged section of long ladder is the flat winged section of cruise starting subsequently into step S18.
It please join Figure 13, in some embodiments, flight visual simulation device 10a further include:
Second judgment module 13, the second judgment module 13 is for judging whether the flat winged section of ladder meets height continuation condition；
Second determining module 15, the second determining module 15 are used to not find the flat winged section of ladder for meeting height continuation condition
When the determining highest nearest from takeoff point or the flat winged section of longest ladder be the flat winged section of cruise starting.
Likewise, it is appreciated that in some embodiments, step S13, S15 can respectively by the second judgment module 13,
Second determining module 15 executes or implements, and the second judgment module 13, the second determining module 15 may be respectively used for holding in other words
Capable or implementation steps S13, S15.
In these embodiments, flight visual simulation method, flight visual simulation device 10a, 100 and of computer system
Computer readable storage medium can also handle some extreme flight progress, and TOC is therefrom accurately positioned.Specifically, general fly
In row situation, the flat winged section for meeting the height continuation condition being rationally arranged can be always found from displacement-altitude curve, and more
Extreme situation, for example, super shorter flight or due to various reasons aircraft constantly climb it is high with satisfaction may be can not find when decline
The flat winged section of duration is spent, it in this case still can be by finding the highest nearest apart from takeoff point or longest flat
Winged section positions TOC.
In the description of this specification, reference term " certain embodiments ", " in an example ", " illustratively " etc. are retouched
It states and means to be contained in the application extremely in conjunction with the embodiment or example particular features, structures, materials, or characteristics described
In a few embodiment or example.In the present specification, schematic expression of the above terms are not necessarily referring to identical
Embodiment or example.Moreover, particular features, structures, materials, or characteristics described can be real in any one or more
Applying can be combined in any suitable manner in mode or example.In addition, without conflicting with each other, those skilled in the art can be with
The feature of different embodiments or examples described in this specification and different embodiments or examples is combined.
Any process described otherwise above or method description are construed as in flow chart or herein, and expression includes
It is one or more for realizing specific logical function or process the step of executable instruction code module, segment or portion
Point, and the range of the preferred embodiment of the application includes other realization, wherein can not press shown or discussed suitable
Sequence, including according to related function by it is basic simultaneously in the way of or in the opposite order, Lai Zhihang function, this should be by the application
Embodiment person of ordinary skill in the field understood.
Although presently filed embodiment has been shown and described above, it is to be understood that above embodiment is
Illustratively, it should not be understood as the limitation to the application, those skilled in the art within the scope of application can be right
Above embodiment is changed, modifies, replacement and variant.
Claims (10)
1. a kind of flight visual simulation method, climbing on displacement-altitude curve of the flight vertical section for positioning aircraft
Vertex, which is characterized in that the flight visual simulation method includes:
Judge whether the displacement-altitude curve includes one Dan Pingfei sections or the flat winged section of multiple ladders；
When including described Dan Pingfei sections, positioning Dan Pingfei sections of the starting point is the vertex of climbing；
When including that multiple ladders equal winged section, determine that first flat winged section of the ladder for meeting height continuation condition is to patrol
Boat starting is flat to fly section, and the height continuation condition refers to that the flat winged section of the cruise starting is higher than predetermined altitude and the duration is greater than pre-
It fixes time；With
The starting point for positioning the flat winged section of the cruise starting is the vertex of climbing.
2. flight visual simulation method according to claim 1, which is characterized in that the judgement displacement-height is write music
Whether line includes the steps that the flat winged section of one Dan Pingfei sections or multiple ladders includes:
Identify that the horizontal line section on the displacement-altitude curve is flat winged section；
Whether the number for judging the flat winged section is 1 or greater than 1；
When the number of the flat winged section is 1, determine that the displacement-altitude curve includes Dan Pingfei sections described；With
When the number of the flat winged section is greater than 1, determine that the displacement-altitude curve includes the flat winged section of multiple ladders.
3. flight visual simulation method according to claim 1, which is characterized in that the height continuation condition includes one
The predetermined altitude and a corresponding predetermined time.
4. flight visual simulation method according to claim 1, which is characterized in that the height continuation condition includes multiple
The predetermined altitude and multiple corresponding predetermined times.
5. flight visual simulation method according to claim 1, which is characterized in that the flight visual simulation method is also wrapped
It includes:
Judge whether the flat winged section of the ladder meets the height continuation condition, when meeting the height continuation condition, enters
The step of flat winged section of the ladder that the determination first meets height continuation condition originates flat winged section for cruise；
When not finding the flat winged section of the ladder for meeting the height continuation condition, the determining highest nearest from takeoff point or most
The flat winged section of the long ladder is flat winged section the opening subsequently into the positioning cruise flat winged section of starting of the cruise starting
Initial point be it is described climb vertex the step of.
6. a kind of flight visual simulation device, climbing on displacement-altitude curve of the flight vertical section for positioning aircraft
Vertex, which is characterized in that the flight visual simulation device includes:
First judgment module, the first judgment module is for judging whether the displacement-altitude curve includes a Dan Pingfei
Section or the flat winged section of multiple ladders；
First locating module, first locating module are used to position described Dan Pingfei sections when including described Dan Pingfei sections and open
Initial point is the vertex of climbing；
First determining module, first determining module are used to include that multiple ladders determine first satisfaction when equalling winged section
The flat winged section of the ladder of height continuation condition is the flat winged section of cruise starting, and the height continuation condition refers to that the cruise starting is flat
Fly section higher than predetermined altitude and the duration is greater than the predetermined time；With
Second locating module, the starting point that second locating module is used to position the flat winged section of the cruise starting is described climbs
Vertex.
7. flight visual simulation device according to claim 1, which is characterized in that the flight visual simulation device also wraps
It includes:
Second judgment module, second judgment module continue item for judging whether the flat winged section of the ladder meets the height
Part；
Second determining module, second determining module are used for not find the ladder that meets the height continuation condition flat
Flying the determining highest nearest from takeoff point or the longest ladder flat winged section when section is the flat winged section of cruise starting.
8. a kind of computer system, which is characterized in that the computer system includes processor, and the processor is used for:
Judge whether the displacement-altitude curve includes one Dan Pingfei sections or the flat winged section of multiple ladders；
When including described Dan Pingfei sections, positioning Dan Pingfei sections of the starting point is the vertex of climbing；
When including that multiple ladders equal winged section, determine that first flat winged section of the ladder for meeting height continuation condition is to patrol
Boat starting is flat to fly section, and the height continuation condition refers to that the flat winged section of the cruise starting is higher than predetermined altitude and the duration is greater than pre-
It fixes time；With
The starting point for positioning the flat winged section of the cruise starting is the vertex of climbing.
9. a kind of computer system, which is characterized in that the computer system includes:
One or more processors, memory；
One or more programs, wherein one or more of programs are stored in the memory, and one
Or multiple processors execute, described program includes for executing at flying quality described in -5 any one according to claim 1
The instruction of reason method.
10. a kind of non-volatile computer readable storage medium storing program for executing comprising computer-readable instruction, the computer-readable instruction
When being executed by processor, so that the processor executes flight visual simulation side described in -5 any one according to claim 1
Method.
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| CN112596890A (en) * | 2021-01-08 | 2021-04-02 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Flight program operation logic structuring method and system |
| CN113625741A (en) * | 2021-09-01 | 2021-11-09 | 北京北航天宇长鹰无人机科技有限公司 | Flight segment control method and device |
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