In this paper, the problem of finding the optimal trajectory of an aircraft through a specified airspace for a given start and goal position is put forward. The application of sequential programming to optimal trajectory generation is reported with the selection of the grid size and the space boundaries. A totally discrete approach is adopted in contrast to the other models, which use continuous time but resort to diseretization in the computation. The component of the mathematical formulation of the optimization criteria is considered and the procedures used within the control algorithm on the solution are also proposed. Realistic constraints such as turning rate and spatial layout are incorporated into the system model building before applying the sequential programming technique to be used in solving the problem. Simulation examples for multiple aircrafts are presented to demonstrate the use of the proposed trajectory planner and certain optimal control inputs have been acquired.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Development of a new tool for constrained conflict resolution


    Contributors:


    Publication date :

    2019-04-01


    Size :

    12 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






    RESOLUTION OF ROUTE CONFLICT

    VARKKI ANSSI / ÅSTRÖM JANI | European Patent Office | 2016

    Free access

    Aircraft conflict resolution cataloguer

    Yao, Chu / Rusu, Adrian / Danick, Andrew et al. | IEEE | 2017


    Automated conflict resolution issues

    Wike, Jeffrey S. | NTRS | 1991