An output feedback control law is presented, hereafter called the line
ar quadratic coupled delay compensator (LQCDC), for application to pro
cesses that are subjected to randomly varying distributed delays. An e
xample is future generation aircraft, which are equipped with computer
networks to serve as the communications link for the vehicle manageme
nt system. The LQCDC is synthesized via dynamic programming in the sto
chastic setting. A pair of discrete-time modified matrix Riccati equat
ions and a pair of modified matrix Lyapunov equations are constructed
by using lagrangian multipliers and the matrix minimum principle. The
performance cost is formulated as the conditional expectation of a qua
dratic functional adjoined with an equality constraint involving the d
ynamics of the conditional covariance of the closed-loop system state.
Results of simulation experiments are presented to demonstrate the ef
ficacy of the LQCDC for control of longitudinal motion of an advanced
aircraft.