Continuous time-predictive control approach is employed to formulate an output tracking nonlinear, optimal, terminal guidance law for re-entry vehicles. The notable features of this formulation are that the system equations are not linearised and the evaluation of the guidance equations does not need the information of vehicle parameters, such as drag and mass. The formulation allows to impose the physical constrains on the control inputs, i.e. on the demanded lateral accelerations through a saturation mapping and the controls are obtained using a fixed point iteration algorithm which converges typically in a few iterations. Further, a simple method of tuning the prediction horizon needed in the guidance equations is presented. Numerical si...
The guidance and control algorithms for enabling spacecraft proximity operations about small celesti...
International audienceThis paper addresses the implementation of a predictive control strategy for U...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.In...
Continvojs time-predictive control approach is employed to formulate an output tracking nonlinear, o...
This paper discusses a new nominal riding reentry guidance law design based on a nonlinear optimal p...
This Paper discusses a new nominal riding reentry guidance low design based on a nonlinear optimal p...
The problem of reentry guidance for an atmospheric entry vehicle is taken up for the study with focu...
A guidance scheme has been developed which provides for the terminal guidance of an unpowered liftin...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.In...
A nonlinear suboptimal guidance scheme is developed for the reentry phase of the reusable launch veh...
In this work, a centralised robust model predictive control (CRMPC) algorithm is proposed for reentr...
A new guidance philosophy by introducing a trajectory dependent variable guidance gain in the predic...
It is observed that general explicit guidance schemes exhibit numerical instability close to the inj...
A robust suboptimal reentry guidance scheme is presented for a reusable launch vehicle using the rec...
This work aims to demonstrate the benefits and limitations of an on-board Guidance for reusable laun...
The guidance and control algorithms for enabling spacecraft proximity operations about small celesti...
International audienceThis paper addresses the implementation of a predictive control strategy for U...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.In...
Continvojs time-predictive control approach is employed to formulate an output tracking nonlinear, o...
This paper discusses a new nominal riding reentry guidance law design based on a nonlinear optimal p...
This Paper discusses a new nominal riding reentry guidance low design based on a nonlinear optimal p...
The problem of reentry guidance for an atmospheric entry vehicle is taken up for the study with focu...
A guidance scheme has been developed which provides for the terminal guidance of an unpowered liftin...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.In...
A nonlinear suboptimal guidance scheme is developed for the reentry phase of the reusable launch veh...
In this work, a centralised robust model predictive control (CRMPC) algorithm is proposed for reentr...
A new guidance philosophy by introducing a trajectory dependent variable guidance gain in the predic...
It is observed that general explicit guidance schemes exhibit numerical instability close to the inj...
A robust suboptimal reentry guidance scheme is presented for a reusable launch vehicle using the rec...
This work aims to demonstrate the benefits and limitations of an on-board Guidance for reusable laun...
The guidance and control algorithms for enabling spacecraft proximity operations about small celesti...
International audienceThis paper addresses the implementation of a predictive control strategy for U...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.In...