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参考文献 1
CHATTERJRG B, SRIDHARB . Measures for air traffic controller workload prediction[C] //Proceedings of the 1st AIAA Aircraft, IntegrationTechnology , and ForumOperations . California:[s.n.],2001.
参考文献 2
GIANAZZAD . Airspace configuration using air traffic complexity metrics[C]//7th USA/Europe ATM R&D Seminar. Barcelona, Spain: s.n.], 2007.
参考文献 3
DJOKICJ, LORENZB, FRICKEH . Air traffic control complexity as workload driver[J]. Transportation Research Part C: Emerging Technologies, 2010,18(6): 930⁃936.
参考文献 4
KOPARDEKARP, SCHWARTZA, MAGYARITSS, et al . Airspace complexity measurement: An air traffic control simulation analysis[C]//7th USA/Europe ATM R&D Seminar. Barcelona, Spain: s.n.], 2007.
参考文献 5
KOPARDEKARP, MAGYARITSS . Dynamic density: Measuring and predicting sector complexity[C]//Proceedings of the 21st Digital Avionics Systems Conference, IEEE. Piscataway, New Jersey: IEEE, 2002.
参考文献 6
TOY J . Complexity metric comparison study for controller workload prediction in 4D trajectory management environments[D]. Delft: Delft University of Technology, 2015.
参考文献 7
NETJASOVF . Terminal airspace traffic complexity[D]. Belgrade: University of Belgrade, 2004.
参考文献 8
SONGZ X, CHENY Z, LIZ L, et al . A review for workload measurement of air traffic controller based on air traffic complexity[C]//25th Control and Decision Conference (CCDC). [ S .l.]: IEEE, 2013: 2107⁃2112.
参考文献 9
DELAHAYED, PUECHMORELS . Air traffic complexity: Towards an intrinsic metric[C]//3rd USA/Europe ATM R&D Seminar. Napoli: s.n.], 2000.
参考文献 10
DELAHAYED, PAIMBLANCP, PUECHMORELS, et al . A new air traffic complexity metric based on dynamical system modelization[C]//21st Digital Avionics Systems Conference. Irvine, CA, USA: IEEE, 2002.
参考文献 11
YEB J, ZHANGJ, HUM H, et al . Modeling of air traffic complexity based on traffic structure[J]. Journal of Transportation Systems Engineering and Information Technology, 2012,12(1): 166⁃172. (in Chinese)
参考文献 12
XUX H, HUANGB J, SHUQ . Evaluation of sector complexity based on intrinsic attributes[J]. Journal of Civil Aviation of China, 2013,31(2): 22⁃28. (in Chinese)
参考文献 13
XUX H, LID B, LIX . Study on safety assessment of flight interval[J]. Journal of Aeronautical, 2008,29(6): 1411⁃1418. (in Chinese)
参考文献 14
ZHANGJ, HUM H, ZHANGC . Research on the complexity in air traffic management[J]. Acta Aeronautica et Astronautica Sinica, 2009,11(30): 2132⁃2141. (in Chinese)
参考文献 15
ZHANGJ, HUM H, ZHANGC, et al . Spatial complexity modeling[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2010,42(4): 454⁃460. (in Chinese)
参考文献 16
CHATTERJIG B, SRIDHARB . Measures for air traffic controller workload prediction[C] //1st AIAA Aircraft, Technology, Integration, and ForumOperations . California, Los Angeles: [s.n.], 2001.
参考文献 17
PARIMALK, TOM P, MICHEALJ . Traffic complexity measurement under higher levels of automation and higher traffic densities[C]//AIAA Guidance, Navigation and Control Conference and Exhibit. [ S .l.]:AIAA, 2008.
参考文献 18
EUROCONTROL . Air traffic flow & capacity management operations ATFCM users manual[M]. [ S .l.]: The European Organisation for the Safety of Air Navigation(EUROCONTROL), 2015.
参考文献 19
QIURentian, WANGLong . Acceptable air traffic unevenness model construction[J]. Command Information System and Technology, 2017, 8(2): 77⁃81. (in Chinese)
Document Sections

    Abstract

    It is an important issue to assess traffic situation complexity for air traffic management. There is a lack of systematic review of the existing air traffic complexity assessment methods, and there is no consideration of the role of airspace and traffic coordination mechanism. A new 3⁃D airspace complexity measurement method is proposed based on route structure constraints to evaluate the air traffic complexity objectively. Firstly, the model of the impact on horizontal and vertical direction for "aircraft pair" is established based on the route guidance. After that, the coupled complexity model for 3⁃D airspace is given according to the modification on the model in terms of flight standardization. Finally, the global model of the airspace traffic complexity is established. It is proved by the experimental data from the actual operation in airspace that the proposed model can reflect the space coupling situation and complexity of aircraft. At the same time, it can precisely describe the actual operation of civil aviation in China.

    摘要

    暂无

  • 0 Introduction

    The air traffic system is a complex system formed by the collaboration of airspace structures and traffic flow. The complexity of air traffic depends on the interaction of different aircraft in the airspace. However, the traffic flow made up of aircraft must adapt to the restriction of airspace structure by changing operating characteristics, which in turn leads to a further dynamic evolution of the traffic complexity. To ensure the safety of airspace traffic flow is the primarily responsibility of air traffic controllers. Workload of controllers also directly affects the operation safety of aircraft under their jurisdiction. Therefore, an accurate measurement of the complexity of airspace traffic and a reasonable division of the busyness of the sectors can effectively reduce or control the workload of controllers and ensure the safety of aircraft operations.

    At present, the airspace complexity and the degree of busyness are mainly divided by methods based on the amount of flights, ignoring the impact of airspace structure on aircraft operation. In fact, the airspace route structure will have a serious impact on the air traffic flow in two inspects: The guiding influence will affect the trend of traffic flow and the restrictive effect, which means the traffic flow must fly along the specified route and meet its operating standards. However, due to the complexity of the relationship between airspace structure and traffic flow, the accurate assessment of air traffic complexity has become a thorny problem in air traffic management.

    Since the complexity measured by route structure can evaluate the traffic flow status more comprehensively, this paper proposes a complexity calculation model based on "aircraft pair", after analyzing the guidance and normative constraints of the airspace route structure to the aircraft and evaluates the overall complexity of the airspace. The proposed model can reveal the process of traffic complex situation changing from one “aircraft pair” to multiple “aircraft pair” environment, and evaluate the complexity of the air traffic more objectively.

  • 1 Related Work

    In recent years, domestic and foreign scholars have carried out a series of researches on the issue of air traffic complexity and made some achievements.

    Focusing on the impact of air traffic complexity on controller’s workload, Chatterjr et al.[1] analyzed and expanded the factors affecting traffic complexity and studied the nonlinear relationship between controller’s workload and traffic flow complexity. Gianazza[2] studied the relationship between air traffic complexity and controller’s workload based on artificial neural network and put forward the idea of airspace division based on traffic complexity. Djokic et al.[3] analyzed the components of air traffic complexity and analyzed the relationships among various factors affecting traffic complexity by clustering and regression analysis. Jelena also defined task requirements and regulatory behaviors, and studied the relationship between traffic complexity and controller’s workload.

    Focusing on the idea of dynamic density, Kopardekar et al.[4,5] proposed the concept of dynamic density, which considers dynamic density as a set of all factors that affect the complexity of air traffic. Toy[6] built two models of traffic behavior complexity assessment: One modeling approach based on dynamic density, including the number of aircraft, the reciprocal of the average weighted horizontal interval, the reciprocal of the minimum horizontal interval, the standard deviation of velocity, the average difficulty of conflict resolution and other factors; the other is based on the complexity of the trajectory measurement, taking into account sector size, weather effects, violation of standard intervals and other factors.

    Focusing on the static and dynamic factors, Netjasov[7] studied the traffic complexity in the terminal area and concluded that the traffic complexity was caused by the combination of the static factors of the airspace structure and the dynamic characteristics of the traffic flow. The static elements of airspace structure include the distribution of flight segments in airspace, the degree and number of intersections, etc. The dynamic characteristics of traffic flow include the distribution of flights on each flight segment, and the number of aircraft changing altitude, etc. Song et al.[8] summarized the research on air traffic complexity and concluded that the complexity factors include both static and dynamic ones. Static factors generally have less change, including routes, airports and so on. Dynamic factors include changes in the status of the aircraft itself or regulatory instructions.

    Focusing on the dynamic factors of aircraft, Delahaye et al.[9,10] objectively described the changes in complexity by using the aircraft’s intrinsic attribute, such as speed and heading, constructed a traffic disorder model and analyzed its complexity. However, in the description of the overall traffic situation, the simple addition of single aircraft was considered, but the interaction between aircraft was ignored. Therefore the coupling complexity cannot be accurately explained. Based on the route structure, Ye et al.[11] defined two complexity factors: Distance and conflict to reflect the influence of the relative distance between aircraft and the cross⁃track interaction on the complexity. Xu et al.[12,13] established a complexity measurement model which took into account the approach time, aggression function, relation matrix, correlation function and other dynamic factors of “aircraft pair”.

    It is noteworthy that the domestic scholar Zhang is committed to a study of airspace traffic complexity in recent years and has achieved some significant results. They reviewed the researches of complexity, analyzed the advantages and disadvantages of different models, and focused on the theoretical achievements in dynamic density, traffic chaos and the modeling of complex systems in airspace[14]. They studied the disorder and perturbation of air traffic flow and constructed a spatial complexity model based on intrinsic complexity[15]. They studied the interaction of "aircraft pair" in a two⁃dimensional airspace and used the inner product of the relative velocity vector and the relative position vector of the "aircraft pair" to determine the situation of the two aircraft. When two aircraft are in a state of convergence, it is considered to be a conflict tendency at the time. However, the conclusions reached by this method are still different from the actual operation, which may be explained by the following two reasons. One is that the relative movement tendency of "aircraft pair" is not only related to its own relative position and relative speed, but also influenced by the orientation and restrictiveness of the route structure[16,17,18]. The other is that airspace is three⁃dimensional and the "aircraft pair" situation presented in a single dimension can not determine their conflict. For example, two aircraft at different levels in same route, seem to converge in the horizontal direction, and there is no conflict between them[19].

    Inspired by the above work, this paper attempts to establish a three⁃dimensional traffic complexity measurement model for the entire airspace based on the interaction between aircraft and the impact of route structure on "aircraft pair".

  • 2 Complexity Model of "Aircraft Pair" Based on Route Structure

  • 2.1 Constrain of route structure to aircraft

    To regulate and guide traffic, route structure constrains and limits the aircraft’s flying path to make the traffic from disordered to ordered and to reduce the complexity of the overall traffic situation. If the aircraft within the sector deviates from the prescript route, the traffic complexity will increase sharply, thereby increasing the workload of the controllers. In Fig.1, aircraft “a” in the horizontal direction satisfies the route constraint, however, aircraft “b” and “c” deviate from the prescript route. Although aircraft “d” is on the route, there is a tendency to deviate from the prescribed flight direction. After a period, it may deviate from the original route and no longer comply with the restrictions of airspace structures. The relationship between aircraft “d” and other aircraft may be changed from the original conflict⁃free interaction to an expected conflict⁃like interaction, which not only increases the complexity of the entire transportation system but also brings about the potential safety hazard of air traffic.

    Fig.1
                            Constrain of route structure to aircraft

    Fig.1 Constrain of route structure to aircraft

  • 2.2 “Aircraft pair” interaction model

  • 2.2.1 Aircraft pair

    In three⁃dimensional space, the relative movement between the aircraft can be divided into convergence and dispersion, and the dynamic relationship between aircraft determines whether there are conflicts and security threats in traffic flow. To facilitate the description of aircraft⁃to⁃aircraft relationships, any two aircraft within a particular airspace are defined as "aircraft pair". The traffic complexity mainly depends on the interaction between different "aircraft pair" and the consistency of traffic flow, such as the similarity of each "aircraft pair" in the airspace.

    To reveal the emergence of traffic complexity from a single "aircraft pair" to a multi⁃aircraft environment, it is necessary to set out from the microscopic relationship of "aircraft pair" and establish interaction models for conflict⁃expected state and conflict⁃free state. Based on these two models, we can further consider the correction of the route structure to the model, and finally construct a model to describe the overall complexity of the airspace.

  • 2.2.2Interaction model of conflict⁃expected

    Assuming that the minimum over⁃time interval for a waypoint is STsep , the relative position between two aircraft is Dij and their speeds are Vi and Vj (vectors). Then, the minimum safety distance is: Dsep=Vi-Vj·STsep and the time for aircraft i flighting from the conflict point to the estimated collision point can be presented by following expression

    STi=DsepVi=Vi-Vj·STsepVi
    (1)

    Conflicts occur when either one of the two aircraft arrives at the collision point. The approaching factor is presented as

    Tij=STsep·STijSTsepαα1
    (2)

    where STij=minSTi,STj . Then the "aircraft pair" interaction model in the horizontal direction can be constructed as

    LvlPairij=e-λ·Tij=e-λ·STsep·STijSTsepα
    (3)

    where λ>0 and α>0 are the complexity adjustment parameters of horizontal direction(discussed in Section 2.3.3). It can be seen from the formula that the horizontal complexity LvlPairij will increase exponentially with the decrease of Tij , that is, the closer the aircraft is to the collision point, the more horizontal traffic complexity will sharply increase.

    For the interaction of "aircraft pair" in vertical direction, since only the current relative speed and relative position of aircraft are related, the interaction model can be expressed as

    VerPairij=e-μHDsep·HDijHDij,HVijHDijHDsepβ
    (4)

    where β>0 and μ>0 are the complexity adjustment parameters of vertical (discussed in Section 2.3.3). HDsep is the vertical minimum safety distance, HDij and HVij are vertical relative distance and relative speed. It can be seen from the formula that the vertical complexity VerPairij increases exponentially with the increase of relative velocity HVij and the decrease of relative position HDij . That is, the greater the relative speed, the closer the distance, the more vertical traffic complexity will sharply rise.

  • 2.2.3Interaction model of conflict⁃free

    When two aircraft are in a conflict⁃free state, the convergence and dispersion of "aircraft pair" in horizontal and vertical directions will still affect the overall traffic complexity. In horizontal direction, the discrete stress is mainly reflected by the time of the aircraft near or away from the convergence point. The discrete stress model is constructed as

    Tij=1+STijSTsepeα1-STi-STjSTi2+STj2
    (5)

    where α0 STij=minSTi,STj is the equivalent approaching factor. STi and STj represent the time of two aircraft from the convergence point. If there is no convergence point, the “aircraft pair” is considered as irrelevant, STi,STj are infinite, and the mutual influence is set to 0.

    The interaction model of the "aircraft pair" in the horizontal direction is as

    LvlPairij=e-λTij=e-λ1+|STij|STsepeα1-|STi-STj|STi2+STj2
    (6)

    The interaction model of the "aircraft pair" in the vertical direction is represented as

    VerPairij=e-μ|HDij|HDsepeβ(HDij,HVij)
    (7)

    where β>0,μ>0 .The definition and value of λ , α , β and μ are the same as the previous ones.

  • 2.3 Model correction based on route constraints

  • 2.3.1 Normative model

    The normative degree of an aircraft refers to the conformity between the trajectory profile of an aircraft and the prescribed route, in both horizontal and vertical directions. For the norms in the horizontal direction, the horizontal offset distance between the flight track of the aircraft and the route and the degree of fluctuation of the flight track of the aircraft in horizontal plane should be considered. Therefore, the aircraft’s horizontal normative model can be constructed as

    LevelNormi=11+LvlDiviLDsepτeωLvlVARi
    (8)

    where LvlDivi is the average distance of the flight track deviating from the route in horizontal plane in previous period. LDsep is the width of the protection zone. LvlVARi is the deviation variance of the flight track from the route in horizontal plane in previous period. It can be concluded that the greater the distance deviation or fluctuation, the lower the normative degree of the flight.

    Aircraft movements in vertical direction are in two kinds: Cruise, climb or descend. When the aircraft cruises, its vertical normative is mainly described by its offset and volatility in vertical direction. The model is expressed as

    VerticalNormi=1/1+VerDiviVDsepρeσVerVARi
    (9)

    When the aircraft climbs or descends, its vertical normative is mainly described by its volatility in vertical direction. The model is expressed as

    VerticalNormi=1/eσVerCVARi
    (10)

    where VerDivi is the average distance value of the flight track deviating from the route in vertical plane in previous period. VDsep is the height of the protection zone. VerVARi is the deviation variance of the flight track from the route in vertical plane in previous period. VerCVARi represents the deviation variance of the climb rate (descent rate) from the planned climb rate (descent rate) in previous period. τ,ω,ρ,σ are adjustment parameters, τ,ρ1 . It can be concluded that the larger the offset distance or the fluctuation, the lower the normative degree of the flight, and the closer the value of VerticalNormi is to 1, the stronger the ability of the aircraft to fly along the route during the previous period.

  • 2.3.2 Model correction

    Based on the definition of flight normative in last section, the correction parameters LAPij and VAPij for "aircraft pair" (i,j) in the horizontal and vertical directions can be defined as

    LAPij=LevelNormiLevelNormj
    (11)
    VAPij=VerticalNormiVerticalNormj
    (12)

    The range of LAPij and VAPij is (0,1). The closer the value is to 1, the better the flight normative and stability.

    Therefore, for the "aircraft pair" (i,j) in conflict⁃expected state, the corrected interaction models in horizontal and vertical directions can be expressed as

    LvlAdjPairij=e-λLAPijSTsepSTijSTsepα
    (13)
    VerAdjPairij=e-λVAPijHDsepHDij|HDij,HVij|HDij|HDsepα
    (14)

    where λ>0,α1 .

    For the "aircraft pair" (i,j) in conflict⁃free state, the corrected interaction models in horizontal and vertical directions can be expressed as

    LvlAdjPairij=e-μLAPij1+|STij|STsepeβ1-|STi-STj|STi2+STj2
    (15)
    VerAdjPairij=e-μVAPijHDijHDsepeβHDij·HVij
    (16)

    where β>0,μ>0 .

  • 2.3.3 Parameters in models

    The approaching effect in the horizontal and vertical directions are divided into four levels: low, medium, high and very high, as shown in Table1. The key parameters λ,α,μ,β of the models have different values referring to the level of approaching effect, as shown in Table2.

    Table 1 Approaching effect levels

    Horizontal approaching
    Relative distance/kmRelative velocity/(km·h-1
    <370<1 050<1 480≥1 480
    ≥130LowLowLowMedium
    <130LowLowLowMedium
    <75LowLowMediumHigh
    <45LowMediumMediumHigh
    <20MediumHighVery highVery high
    Vertical approaching
    Relative distance/mRelative velocity/(m·s-1
    <6<13<16≥16
    ≥1 200LowLowLowMedium
    <1 200LowLowMediumMedium
    <900LowLowMediumHigh
    <600LowMediumMediumHigh
    <300MediumHighVery highVery high

    Table 2 Value of model parameters

    Horizontal complexity parameterHorizontal Proximity levelVertical complexity parameter

    Vertical Proximity

    level

    λ1 21.774Low μ1 41.548Low
    λ2 0.249Medium μ2 0.478Medium
    λ3 0.043High μ3 0.082High
    λ4 0.914Very high μ4 1.728Very high
    α1 1Low β1 0.010 0Low
    α2 2Medium β2 0.000 4Medium
    α3 3High β3 0.001 0High
    α4 4Very high β4 0.000 2Very high
  • 3 Complexity Model of Global Traffic

    From "Barrel Theory", we know that the overall capacity of a system is determined by the least capable component. Therefore, the interaction between two aircraft is important to the overall traffic complexity in two dimensions. To integrate the interactions in horizontal and vertical directions, a coupling parameter is defined as

    CAdiParaij=1-LvAdjPairij-VerAdjPairijLvAdjPairij2+VerAdjPairij2
    (17)

    The formula shows that the weaker one will weaken the impact of the stronger one. Therefore, the stronger one needs to be adjusted by the coupling parameter. Thus, the coupling complexity model for "aircraft pair" (i,j) is shown as

    Pairij=LvlAdjPairij+CAdjParaijVerAdjPairijVerAdjPairij>LvlAdjPairijVerAdjPairij+CAdjParaijLvlAdjPairijElse
    (18)

    As we know there are often several "aircraft pairs" in an airspace simultaneously. If there is an "aircraft pair" conflict, the complexity of the entire airspace will increase. Since the global traffic has different effect to each "aircraft pair", we should firstly calculate the weight. The weight may meet the following conditions: The weight needs to be proportional to the interaction of an "aircraft pair", and the global traffic will have an impact on every aircraft in it. The impact function is

    RevPairi=j=1NPairijParaij
    (19)

    where the weight is calculated as

    Paraij=PairijkiPrikij0i=j
    (20)

    The weights reflect the differences of global traffic impact on any of its aircraft. The impact difference between aircraft i and j caused by global traffic can be calculated as

    Distinctij=|Paraij-Paraji|/(Paraij2+Paraji2)
    (21)

    Based on the degree of difference, the concept of similarity can be defined as

    Similarityij=(1-Distinctijρ)1θ
    (22)

    where ρ and θ are adjustment parameters. The similar degree of impact of aircraft i and j reflects the relative impact of each aircraft on the overall traffic, that is the traffic consistency.

    For airspace with N aircraft, its global traffic complexity can be presented as

    Complexity=i=1N(RevPairij=1,jiNSimilarityij)
    (23)

    The model takes into account the impact of global traffic on each aircraft and the similarity between the aircraft.

  • 4 Case Analysis

    To verify the validity of the proposed complexity models, we apply them on the actual flight operation data and spatial structure data of Guangzhou 03 sectors to calculate the airspace complexity.

  • 4.1 Analysis of the sector complexity

    On the data from Guangzhou 03 Sector on October 11, 2017 from 15:00 to 16:00, the airspace complexity in this period is evaluated. Fig.2shows the static structure of Guangzhou 03 sector. Fig.3shows the relationship between the real⁃time complexity of the sector and the number of aircraft in the sector during the statistical period with the statistics interval 1 min.

    Fig.2
                            Guangzhou 03 sector structure

    Fig.2 Guangzhou 03 sector structure

    Fig.3
                            Relationship between airspace complexity and aircraft amount

    Fig.3 Relationship between airspace complexity and aircraft amount

    In Fig.3, 15:36 and 15:38 have the same flight amount, but the complexity is different. Compare the distribution of traffic patterns at 15:36 and 15:38, as shown in Figs.4(a,b), it can be seen that a convergence is occurring in Fig.4(b), so that the calculated traffic complexity of 15:38 is higher than 15:36. Similarly, the flight amount of 15:40 is greater than that of 15:38 but its complexity is smaller than that of 15:38, because although the number of flights is more at 15:40, the convergence tends is more moderate. It can be seen that the computational model of airspace complexity proposed in this paper can objectively and accurately reflect the impact of flight amount and traffic conditions on the airspace complexity.

    Fig.4
                            15:36 and 15:38 traffic distributions of Guangzhou 03 sector

    Fig.4 15:36 and 15:38 traffic distributions of Guangzhou 03 sector

  • 4.2 Influence of track deviation on complexity

    In practice, factors such as navigation accuracy, meteorological conditions, and pilot capabilities may cause the trajectory of the aircraft to deviate from the actual route, which increases the risk of aircraft operation,and also affects the accuracy of the controller’s predictions of traffic scenario evolution. To verify the influence of track deviation on airspace complexity, based on the data of Guangzhou 03 sector on October 11, 2017 from 15:00 to 16:00, the complexity of corrected track and uncorrected track are calculated, as shown in Fig.5.

    Fig.5
                            Influence of track deviation on complexity

    Fig.5 Influence of track deviation on complexity

    As can be seen from Fig.5, the complexity of corrected track is not lower than that of uncorrected track. Especially around 15:38, the complexity of corrected track is greatly deviated from that of the uncorrected track. ZGGGAR03 sector reproduced 15:38 traffic scenario by processing radar data, as shown in Fig.4(b). At this moment, the flight track of multiple flights in the airspace obviously deviates from the planned route, so the increase of airspace complexity is in line with the actual operation.

  • 5 Conclusions

    This paper proposes a new three⁃dimension airspace complexity measurement method. Compared with other existing related works, the contribution of this paper can be summarized as follows: For the first time, considering the micro⁃realistic factor that the aircraft is constrained by the route, this paper proposes the concept of route guidance and flight norms and a three⁃dimensional coupled model of the "aircraft pair" based on this concept, and then establishes a three⁃dimensional air traffic complexity model. According to the experimental results of actual airspace operation data, the computational model of airspace complexity presented in this paper can truly reflect the aircraft coupling situation and its complexity, and is more suitable for the actual operation of civil aviation in China.

  • References

    • 1

      CHATTERJR G B, SRIDHAR B . Measures for air traffic controller workload prediction[C] //Proceedings of the 1st AIAA Aircraft, Technology Integration , and Operations Forum . California:[s.n.],2001.

    • 2

      GIANAZZA D . Airspace configuration using air traffic complexity metrics[C]//7th USA/Europe ATM R&D Seminar. Barcelona, Spain: s.n.], 2007.

    • 3

      DJOKIC J, LORENZ B, FRICKE H . Air traffic control complexity as workload driver[J]. Transportation Research Part C: Emerging Technologies, 2010,18(6): 930⁃936.

    • 4

      KOPARDEKAR P, SCHWARTZ A, MAGYARITS S, et al . Airspace complexity measurement: An air traffic control simulation analysis[C]//7th USA/Europe ATM R&D Seminar. Barcelona, Spain: s.n.], 2007.

    • 5

      KOPARDEKAR P, MAGYARITS S . Dynamic density: Measuring and predicting sector complexity[C]//Proceedings of the 21st Digital Avionics Systems Conference, IEEE. Piscataway, New Jersey: IEEE, 2002.

    • 6

      TOY J . Complexity metric comparison study for controller workload prediction in 4D trajectory management environments[D]. Delft: Delft University of Technology, 2015.

    • 7

      NETJASOV F . Terminal airspace traffic complexity[D]. Belgrade: University of Belgrade, 2004.

    • 8

      SONG Z X, CHEN Y Z, LI Z L, et al . A review for workload measurement of air traffic controller based on air traffic complexity[C]//25th Control and Decision Conference (CCDC). [ S .l.]: IEEE, 2013: 2107⁃2112.

    • 9

      DELAHAYE D, PUECHMOREL S . Air traffic complexity: Towards an intrinsic metric[C]//3rd USA/Europe ATM R&D Seminar. Napoli: s.n.], 2000.

    • 10

      DELAHAYE D, PAIMBLANC P, PUECHMOREL S, et al . A new air traffic complexity metric based on dynamical system modelization[C]//21st Digital Avionics Systems Conference. Irvine, CA, USA: IEEE, 2002.

    • 11

      YE B J, ZHANG J, HU M H, et al . Modeling of air traffic complexity based on traffic structure[J]. Journal of Transportation Systems Engineering and Information Technology, 2012,12(1): 166⁃172. (in Chinese)

    • 12

      XU X H, HUANG B J, SHU Q . Evaluation of sector complexity based on intrinsic attributes[J]. Journal of Civil Aviation of China, 2013,31(2): 22⁃28. (in Chinese)

    • 13

      XU X H, LI D B, LI X . Study on safety assessment of flight interval[J]. Journal of Aeronautical, 2008,29(6): 1411⁃1418. (in Chinese)

    • 14

      ZHANG J, HU M H, ZHANG C . Research on the complexity in air traffic management[J]. Acta Aeronautica et Astronautica Sinica, 2009,11(30): 2132⁃2141. (in Chinese)

    • 15

      ZHANG J, HU M H, ZHANG C, et al . Spatial complexity modeling[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2010,42(4): 454⁃460. (in Chinese)

    • 16

      CHATTERJI G B, SRIDHAR B . Measures for air traffic controller workload prediction[C] //1st AIAA Aircraft, Technology, Integration, and Operations Forum . California, Los Angeles: [s.n.], 2001.

    • 17

      PARIMAL K, TOM P, MICHEAL J . Traffic complexity measurement under higher levels of automation and higher traffic densities[C]//AIAA Guidance, Navigation and Control Conference and Exhibit. [ S .l.]:AIAA, 2008.

    • 18

      EUROCONTROL . Air traffic flow & capacity management operations ATFCM users manual[M]. [ S .l.]: The European Organisation for the Safety of Air Navigation(EUROCONTROL), 2015.

    • 19

      QIU Rentian, WANG Long . Acceptable air traffic unevenness model construction[J]. Command Information System and Technology, 2017, 8(2): 77⁃81. (in Chinese)

  • Author contributions & Acknowledgements

    Dr. XIE Hua designed the complexity model and guided the case study. Mr. WU Zhe conducted the analysis and wrote the manuscript. Mr. CHEN Feifei contributed to the discussion and the background of this study. Dr. CHEN Haiyan participated in the discussion of the experiments and the result analyses. All authors commented on the draft and approved the submission.

    Acknowledgements:This work was supported by the National Natural Science Foundation of China (No.61573181); the Civil Aviation Joint Fund Key Projects of National Natural Science Foundation of China (No.U1333202).

    Competing Interests

    The authors declare no competing interests.

XIEHua

Affiliation: College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, P.R. China

Profile:Dr.XIE Huareceived his B.S. and M.S. degrees in computer science and the Ph.D. degree in System Engineering from Nanjing University of Aeronautics and Astronautics (NUAA) in 1999, 2005 and 2015, respectively. He is currently a lecturer at College of Civil Aviation, NUAA. His research interests include air traffic flow management and security technology.Mr

WUZhe

Affiliation: College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, P.R. China

Role:Corresponding author

Email:wuzhe0303@aliyun.com.

Profile:E⁃mail address:wuzhe0303@aliyun.com.

CHENFeifei

Affiliation: State Key Laboratory of Air Traffic Management System and Technology, Nanjing 210007, P.R. China

Profile: CHEN Feifeireceived his B.S. and M.S. degrees in transportation planning and management from NUAA in 2012 and 2015, respectively. He is currently a researcher of State Key Laboratory of Air Traffic Management System and Technology. His research interests include air traffic flow management.Dr

CHENHaiyan

Affiliation: College of Computer Science and Technology, Nanjing University of Aeronautics and Astronautics,Nanjing 211106, P.R. China

Profile: CHEN Haiyanreceived her B.S. and Ph.D. degrees in computer science from NUAA in 2003 and 2012, respectively. She is now a lecturer at College of Computer Science and Technology, NUAA. Her research interests include machine learning, data mining, and air traffic flow management.

Sun Jing

Role:Editor

html/njhkhten/201902018/alternativeImage/246b50bd-9ef8-4813-a319-6c9ac6b1c181-F001.jpg
Horizontal approaching
Relative distance/kmRelative velocity/(km·h-1
<370<1 050<1 480≥1 480
≥130LowLowLowMedium
<130LowLowLowMedium
<75LowLowMediumHigh
<45LowMediumMediumHigh
<20MediumHighVery highVery high
Vertical approaching
Relative distance/mRelative velocity/(m·s-1
<6<13<16≥16
≥1 200LowLowLowMedium
<1 200LowLowMediumMedium
<900LowLowMediumHigh
<600LowMediumMediumHigh
<300MediumHighVery highVery high
Horizontal complexity parameterHorizontal Proximity levelVertical complexity parameter

Vertical Proximity

level

λ1 21.774Low μ1 41.548Low
λ2 0.249Medium μ2 0.478Medium
λ3 0.043High μ3 0.082High
λ4 0.914Very high μ4 1.728Very high
α1 1Low β1 0.010 0Low
α2 2Medium β2 0.000 4Medium
α3 3High β3 0.001 0High
α4 4Very high β4 0.000 2Very high
html/njhkhten/201902018/alternativeImage/246b50bd-9ef8-4813-a319-6c9ac6b1c181-F002.jpg
html/njhkhten/201902018/alternativeImage/246b50bd-9ef8-4813-a319-6c9ac6b1c181-F003.jpg
html/njhkhten/201902018/alternativeImage/246b50bd-9ef8-4813-a319-6c9ac6b1c181-F004.jpg
html/njhkhten/201902018/alternativeImage/246b50bd-9ef8-4813-a319-6c9ac6b1c181-F005.jpg

Fig.1 Constrain of route structure to aircraft

Table 1 Approaching effect levels

Table 2 Value of model parameters

Fig.2 Guangzhou 03 sector structure

Fig.3 Relationship between airspace complexity and aircraft amount

Fig.4 15:36 and 15:38 traffic distributions of Guangzhou 03 sector

Fig.5 Influence of track deviation on complexity

image /

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