AIAA Guidance, Navigation, and Control Conference and Exhibit 2001
DOI: 10.2514/6.2001-4294
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Optimal coordinated maneuvers for three dimensional aircraft conflict resolution

Abstract: In this paper, we study the problem of designing optimal coordinated maneuvers for multiple aircraft conflict resolution. We propose an energy function to select among all the conflict-free maneuvers the optimal one. The introduced cost function incorporates a priority mechanism that favors those maneuvers where aircraft with lower priority assume more responsibility in resolving the predicted conflicts. The energy-minimizing resolution maneuvers may involve changes of heading and speed, as well as of altitude… Show more

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Cited by 10 publications
(9 citation statements)
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“…In this formulation of the problem, it is assumed that the intent of the aircraft involved in a conflict scenario is known perfectly, either to a centralized controller, or through the exchange of information through data link between aircraft. In centralized schemes, the central planner chooses the control input of all agents in the conflict scenario to satisfy safety constraints and minimize a global optimality criterion [4], [5].…”
Section: Related Workmentioning
confidence: 99%
“…In this formulation of the problem, it is assumed that the intent of the aircraft involved in a conflict scenario is known perfectly, either to a centralized controller, or through the exchange of information through data link between aircraft. In centralized schemes, the central planner chooses the control input of all agents in the conflict scenario to satisfy safety constraints and minimize a global optimality criterion [4], [5].…”
Section: Related Workmentioning
confidence: 99%
“…There are many existing multi-aircraft trajectory optimi sation methods, most focus purely on cruise-like conditions where trajectories can be approximated in two dimensions or movement in the third dimension is highly penalised for passenger comfort [2]- [4]. Methods such as mixed integer linear progranuning (MILP) require a linearisation of the problem and are too slow on centralised problems with large numbers of vehicles due to the number of binary variables [5].…”
Section: Introductionmentioning
confidence: 99%
“…In this case explicit mathematical solution becomes available [6]. An extension of this method for three dimensional encounters for two aircraft was presented in [3]. This method has not been extended for multiple aircraft encounters.…”
Section: Speeifie Zntroduetionmentioning
confidence: 99%
“…Assuming, each aircraft has a cost function which is defined by integration of square of its speed over the specified maneuver time interval. It has been shown that the least energy for a single aircraft is the constant-speed motion along the line segment from its starting to its destination position [3]. If an aircraft is forced to move along some fixed curve other than a line segment, then the parameterization of the curve with the least energy is the one with constant speed, and the minimal energy is proportional to the square of the curve length.…”
Section: Speeifie Zntroduetionmentioning
confidence: 99%
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