Seyed Hamid Jalali Naini

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

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 is obtained for constant gravity assumption, but it works when the velocitiesto-be-gained are o...

[ 2 ] - Differential Equation of Sensitivity Matrix for Final Velocity Constraint