TL;DR: In this article, the maneuver characteristics of hypersonic glide vehicles are analyzed from the perspectives of maneuver modes and maneuverability, and some performance indices to evaluate the maneuverability are analyzed in.
TL;DR: The flight control system of the Saturn V launch vehicle is discussed in this paper, where attitude/attitude-rate scheme, gain required and stability achieved are discussed. But the attitude/rate scheme is not discussed.
Abstract: Flight control system of Saturn V launch vehicle, discussing attitude/attitude-rate scheme, gain required and stability achieved