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Harmonic and Biharmonic Navigation Functions for Conflict-free Trajectory Planning

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HAL Id: hal-01511749

https://hal-enac.archives-ouvertes.fr/hal-01511749

Submitted on 21 Apr 2017

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Harmonic and Biharmonic Navigation Functions for Conflict-free Trajectory Planning

Laureline Guys, Laurent Lapasset, Virginie Aubreton

To cite this version:

Laureline Guys, Laurent Lapasset, Virginie Aubreton. Harmonic and Biharmonic Navigation Func- tions for Conflict-free Trajectory Planning. SID 2012, 2nd SESAR Innovation Days, Nov 2012, Braun- schweig, Germany. �hal-01511749�

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Harmonic and Biharmonic Navigation Functions for Conflict-free Trajectory Planning

Goal: Compute a trajectory for one aircraft with theoretical proof of static obstacle avoidance.

The obtained trajectories also have to satisfy Air Traffic Management requirements:

Bounded speed

Bounded curvature

Navigation functions

Existing methods

Comparison of trajectories

New method

Speed

Departure Arrival

Departure

Arrival

0 100

10

Evanescent field: the destination is unreachable from some points

The aircraft speed increases when the aircraft comes closer to the destination

Contacts

Laureline Guys - PhD Student - laureline.guys@capgemini.com

Laurent Lapasset - Engineer R&D ATM - laurent.lapasset@capgemini.com Virginie Aubreton - Manager ATM Unit - virginie.aubreton@capgemini.com

Navigation functions are maps of values:

uniformly maximum on the obstacles

minimum at the destination

continuous on the space

By following the decreasing values of the navigation function, the aircraft reaches the destination and avoids all the obstacles.

Harmonic functions satisfy the three properties above and are less-suited to be navigation functions. Their drawback is in the lack of bounds on the speed of the aircraft.

To tackle this problem, we created the Biharmonic Navigation Function .

Harmonic Dirichlet Harmonic Neumann Biharmonic

Constant speed

Example of navigation function

on the space on the space

on the obstacles

Trajectories

Speed profile along the trajectories at the destination

on the space

on the obstacles at the destination on the obstacles

F is the navigation function F is the navigation function

at the destination

Poster2Sesar-2012-1_Fiche RHAccessV2 20/11/12 14:51 Page1

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