Design of a three-axis attitude control system for a spacecraft acted upon by random perturbations Final report
Three axis attitude control system for spacecraft under random perturbations
Friedland, B.↗
Engineering topics
Publications and source records attributed to Sarachik, P. E..
Three axis attitude control system for spacecraft under random perturbations
Mathematical models on stability of attitude control systems acted upon by random perturbation processes
Suboptimal control based on linear changes in vicinity of optimum trajectory
Suboptimal adjoint-vector control theory for linearization of feedback control systems independent of nominal trajectory
Stability problems in randomly excited dynamic systems, discussing partial differential equations governing evolution of conditional probabilities and expectations