An examination is made of the controlled motion of a dynamical system that is subject to interference and is described in the neighborhood of a nominal trajectory by a system of linear equations. It is assumed that the phase vector of the system can be measured exactly only at discrete instants of time. A procedure for constructing a control with simultaneous regard to deviations along two coordinates is proposed on the basis of two guaranteeing controls. This procedure is applied to the problem of constructing the control of an airplane in a vertical plane on landing, in the presence of wind disturbances. Such an approach enables deviations in altitude and vertical velocity simultaneously to be taken into account.
Quasioptimal correction of the motion of an airplane at landing when there are wind disturbances
Quasi-optimale Korrektur der Bewegung eines Flugzeuges bei der Landung bei Stoerungen durch Wind
Soviet Journal of Computer and System Sciences ; 25 , 5 ; 183-188
1987
6 Seiten, 6 Quellen
Aufsatz (Zeitschrift)
Englisch
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