SELF-ADJUSTING SYSTEM WITH NONLINEAR MODEL (SAMONASTRAIVAYUSHCHAYASYA SISTEMA S NELINEINOI MODELYU),
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
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Synthesis of the controller of a nonlinear adaptive system with outside disturbances is described. Control law equations are derived from the original state equations using variational methods. The variables are divided into two basic groups directly observable and nonobservable. The latter are expressed as functions of the first. The problem of flight control of a variable mass body moving in the vicinity of Earth is considered as an example. A set of equations serving as the basis of the control law is derived and a block diagram of a special purpose computer to implement this control law is presented.
- Numerical Mathematics
- Unmanned Spacecraft