Authors: RUSNAK I

Citation: I. Rusnak, CLOSED-FORM SOLUTION FOR THE KALMAN FILTER GAINS OF TIME-VARYING SYSTEMS, IEEE transactions on aerospace and electronic systems, 34(2), 1998, pp. 635-639

Authors: RUSNAK I

Citation: I. Rusnak, EXPONENTIAL CRITERION-BASED GUIDANCE LAW FOR ACCELERATION CONSTRAINEDMISSILE AND MANEUVERING TARGET, Journal of guidance, control, and dynamics, 19(3), 1996, pp. 718-721

Authors: RUSNAK I

Citation: I. Rusnak, CONTROL FOR UNSTABLE NONMINIMUM-PHASE UNCERTAIN DYNAMIC VEHICLE, IEEE transactions on aerospace and electronic systems, 32(3), 1996, pp. 945-951

Authors: RUSNAK I

Citation: I. Rusnak, ADVANCED GUIDANCE LAWS FOR ACCELERATION-CONSTRAINED MISSILE, RANDOMLYMANEUVERING TARGET AND NOISY MEASUREMENTS, IEEE transactions on aerospace and electronic systems, 32(1), 1996, pp. 456-464

Authors: RUSNAK I

Citation: I. Rusnak, ANALYTIC SOLUTION OF THE RICCATI EQUATION FOR THE HOMING MISSILE LINEAR-QUADRATIC CONTROL PROBLEM - COMMENT, Journal of guidance, control, and dynamics, 18(4), 1995, pp. 936-936

Authors: BEZICK S RUSNAK I GRAY WS

Citation: S. Bezick et al., GUIDANCE OF A HOMING MISSILE VIA NONLINEAR GEOMETRIC CONTROL METHODS, Journal of guidance, control, and dynamics, 18(3), 1995, pp. 441-448