SICE Journal of Control, Measurement, and System Integration
Online ISSN : 1884-9970
Print ISSN : 1882-4889
ISSN-L : 1882-4889
Special Issue on SICE Annual Conference 2014
Simultaneous Optimization Method for Trajectory and Sequence for Receding Horizon Guidance in Terminal Area
Daichi TORATANISeiya UENOTakehiro HIGUCHI
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2015 Volume 8 Issue 2 Pages 144-153

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Abstract

The target of this study is to develop the simultaneous optimization method for trajectory and sequence in the airspace near airports (terminal area). Traditionally, the arrival sequence optimization is well studied. However, now it is required that the trajectory is also optimized for the future free flight. In the previous study, the receding horizon guidance (RHG) is developed, and the RHG is able to optimize the trajectory and the sequence. However, this optimization method is able to deal with only two aircraft. In this study, the simultaneous optimization method for trajectory and sequence that is applicable for multiple aircraft by introducing the mixed integer linear programming (MILP) and the continuous method is introduced. The simultaneous optimization method for trajectory and sequence is combined with the RHG. To demonstrate the performance of the RHG with the simultaneous optimization method for trajectory and sequence, the simulation is performed. In this simulation, it is confirmed that the new guidance law is able to optimize the trajectory and the sequence simultaneously and has robustness for uncertainty for time in the terminal area.

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© 2015 The Society of Instrument and Control Engineers
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