AIAA Guidance, Navigation, and Control Conference and Exhibit 2002
DOI: 10.2514/6.2002-4445
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Conflict Detection and Resolution with Traffic Flow Constraints

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Cited by 7 publications
(4 citation statements)
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“…In using a SP formulation, it was necessary for the model to discretize various trajectory variables such as the basic parameters within the discretized regions. It is the purpose of this paper to present a multiobjective optimal trajectory planner, which (1) is based upon the discrete dynamics aircraft model, (2) incorporates the physical constraints of aircraft, (3) compares different forms of cost function to achieve the 13 VS O HV P N M 14 T A H G N M 15 T A H P N M 16 T O H P N M 17 TS O H P N M 18,19 T O H P N M 20 S A H P N M 21 VST O HV P N M 22 TS O H P N M 23 TS O H P N M [24][25][26] T/S O HV P N M 27 TS O H P N M 28 VS O HV P N M 29 VS O HV P N M 30 S O H P N M 31 T O H P N M 32 T O H P N M 33 VS A HV P N M 34 TS O H P N M 35,36 T A H G N M 37, 38 T A H G N M 39, 40 T A H P N M 41 TS O H P N M 42 T O H P N M 43 T O H P N M 44 TS O H P N SP T O H G Y optimal solution, and (4) indicates that the proposed optimization model is flexible enough to handle more general forms of constraint and cost function. The inclusion of spatial grid converts the original trajectory planning model from that of a consecutive program to that of a discrete program, which can be solved, as shown later, rather efficiently and still retains the elegance of the original consecutive programming approach.…”
Section: Problem Statementmentioning
confidence: 99%
“…In using a SP formulation, it was necessary for the model to discretize various trajectory variables such as the basic parameters within the discretized regions. It is the purpose of this paper to present a multiobjective optimal trajectory planner, which (1) is based upon the discrete dynamics aircraft model, (2) incorporates the physical constraints of aircraft, (3) compares different forms of cost function to achieve the 13 VS O HV P N M 14 T A H G N M 15 T A H P N M 16 T O H P N M 17 TS O H P N M 18,19 T O H P N M 20 S A H P N M 21 VST O HV P N M 22 TS O H P N M 23 TS O H P N M [24][25][26] T/S O HV P N M 27 TS O H P N M 28 VS O HV P N M 29 VS O HV P N M 30 S O H P N M 31 T O H P N M 32 T O H P N M 33 VS A HV P N M 34 TS O H P N M 35,36 T A H G N M 37, 38 T A H G N M 39, 40 T A H P N M 41 TS O H P N M 42 T O H P N M 43 T O H P N M 44 TS O H P N SP T O H G Y optimal solution, and (4) indicates that the proposed optimization model is flexible enough to handle more general forms of constraint and cost function. The inclusion of spatial grid converts the original trajectory planning model from that of a consecutive program to that of a discrete program, which can be solved, as shown later, rather efficiently and still retains the elegance of the original consecutive programming approach.…”
Section: Problem Statementmentioning
confidence: 99%
“…TFM handles demand management and typically deals with traffic at the air route traffic control center (ARTCC) level, that is, 10-20 sectors. TFM problems include maintaining the aircraft count in each sector below a specified threshold to ease the human ATC workload, as well as to ensure the safety of the flights [1][2][3][4][5][6][7][8].…”
Section: Introductionmentioning
confidence: 99%
“…Such rate limitations are typically enforced by using miles-intrail or minutes-in-trail restrictions at certain airspace fixes [4] ( [1], chapter 10). As a result, the ATCs face path-planning problems that lie at the interface between traffic flow management and separation assurance [5]. With the exception of the Stream Option Manager of Niedringhaus [6], however, there is little research that integrates in the same framework aircraft separation and metering in order to support this task.…”
mentioning
confidence: 99%
“…IV. Bilimoria and Lee [23] and Mueller et al [5] extend the previously mentioned two-aircraft conflict resolution algorithm [19] to include arrival time and metering constraints. Dugail et al [24] describe the dynamics governing the upstream propagation of sector flow constraints by considering a limited scenario where aircraft velocities and path lengths can be controlled to accommodate an output flow rate restriction in an en route sector.…”
mentioning
confidence: 99%