  Bode integrals of sensitivity and sensitivity-like functions along with
complementary sensitivity and complementary sensitivity-like functions are
conventionally used for describing performance limitations of a feedback
control system. In this paper, we show that in the case when the disturbance is
a wide sense stationary process the (complementary) sensitivity Bode integral
and the (complementary) sensitivity-like Bode integral are identical. A lower
bound of the continuous-time complementary sensitivity-like Bode integral is
also derived and examined with the linearized flight-path angle tracking
control problem of an F-16 aircraft.
