A Simple Explicit Guidance Scheme Based on Velocities-to-be-Gained.

Seyed Hamid Jalali Naini

Volume 8, Issue 1 , March 2011, , Pages 29-36

Abstract
  In this paper, a closedloop strategy in the vertical plane is derived in order to determine the thrust direction of a launch vehicle in terms of velocitiestobe gained The two velocities-to-be-gained are utilized, here, for a given altitude and zero vertical speed in a specied nal time The formulation ...  Read More