A feedforward control technique is presented for the determination of the input/output map associated to the inverse problem of the simulated motion of an aircraft. The procedure is particularly suitable in the redundant cases, which are reduced to nominal ones by imposing physically reasonable constraints on the state variables through a focal optimization algorithm. Comparisons with already available solutions are shown together with some significant applications.
SOLUTION OF AIRCRAFT INVERSE PROBLEMS BY LOCAL OPTIMIZATION / DE MATTEIS, Guido; DE SOCIO, Luciano; Alexander, Leonessa. - In: JOURNAL OF GUIDANCE CONTROL AND DYNAMICS. - ISSN 0731-5090. - STAMPA. - 18:3(1995), pp. 567-571. [10.2514/3.21424]
SOLUTION OF AIRCRAFT INVERSE PROBLEMS BY LOCAL OPTIMIZATION
DE MATTEIS, GUIDO;DE SOCIO, Luciano;
1995
Abstract
A feedforward control technique is presented for the determination of the input/output map associated to the inverse problem of the simulated motion of an aircraft. The procedure is particularly suitable in the redundant cases, which are reduced to nominal ones by imposing physically reasonable constraints on the state variables through a focal optimization algorithm. Comparisons with already available solutions are shown together with some significant applications.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
