In this letter, a floating robotic emulation platform is presented with an autonomous
maneuverability for a virtual demonstration of a satellite motion. Such a robotic platform …

COMPUTATIONAL guidance, which relies extensively on onboard numerical computation to
generate guidance commands in real time, is a great challenge for autonomous applications …

Recent decades have seen a surge in research on trajectory optimization (or optimal
control) as a means of achieving computational guidance, which can be regarded as a …

In this paper, an autonomous optimal guidance algorithm for multi-phase lunar soft landing
is presented. Various stringent requirements of a typical multi-phase soft landing are …

A waypoint constrained multi-phase nonlinear optimal guidance scheme is presented in this
paper for the soft landing of a spacecraft on the Lunar surface by using the recently …

This paper proposes a new computational guidance algorithm using differential dynamic
programming and sparse Gauss-Hermite quadrature rule. By the application of sparse …

This paper proposes a geometric attitude control approach with the model predictive static
programming (MPSP) for a rigid body modeled on the Lie group SO (3). The modeling …

This paper addresses the design of the terminal phase maneuver of the booster landing in
the presence of initial deviations and uncertainties. The primary purpose of this study is to …

A model predictive convex programming (MPCP) on parametrized by trigonometric series
control is proposed in this paper, to solve the optimal control problem of spacecraft attitude …

For achieving the desired configuration of spacecraft at the desired fixed time, a sub-optimal
fixed-finite-horizon configuration control method on the Lie group SE (3) is developed based …