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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1992, Vol. 13 ›› Issue (11): 647-653.

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STATE FEEDBACK LOGIC FOR A CLASS OF REAL TIME DISCRETE EVENT SYSTEM

Li Yong-hua, Gao Wei-bing   

  1. 7 th Research Division,Beijing Univ.of Aeronautics and Astronautics, Beijing, 100083
  • Received:1990-04-03 Revised:1992-03-11 Online:1992-11-25 Published:1992-11-25

Abstract:

In this paper, a new kind of real time discrete event system model is proposed based on the concept of state sojourn times. A definition of real time control-invariance is given for a certain predicate. It is shown that for this class of system, there is a state feedback controller such that the given predicate remains true at the state trajectories of the closed loop system if and only if the given predicate is real time control-invariant. It is also shown that for a given predicate, there is a unique supreme real time control-invariant subpredicate. A procedure is presented for its computation. Finally, an example is given to illustrate the results.

Key words: discrete event systems, state feedback, real time control, control-invariance