Constrained nonlinear receding horizon control and its application to a thrust vectored aircraft

This paper presents a receding horizon control method for input constrained nonlinear systems. The optimization procedure is based on predictions made by incremental models at points made by linearized incremental models eat points of a given seed trajectory and the effect of linearization error are...

সম্পূর্ণ বিবরণ

গ্রন্থ-পঞ্জীর বিবরন
প্রধান লেখক: Lee, Y, Kouvaritakis, B, Cannon, M, IEEE
বিন্যাস: Conference item
প্রকাশিত: 2001