34th Congress of the International Council of the Aeronautical Sciences

06.1 - Flight Dynamics and Control (Control & Modelling)

TRAJECTORY OPTIMIZATION FOR LONG-RANGE AIR-LAUNCHED GLIDING VEHICLES USING CONVEX PROGRAMMING

C.-G. Jung¹, C.-H. Lee¹, M.-J. Tahk¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea

In this paper, trajectory optimization for long-range air-launched gliding vehicles using convex programming is proposed. The dynamics is reformulated to compact form and converted to SOCP problem. Furthermore, the robust convergence is accomplished using the adaptive trust-region method. The proposed method demonstrated rapid and stable convergence of SCP with a crude initial guess.


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