Maneuver-aided active satellite tracking using six-DOF optimal dynamic inversion control

Y Li, Z Jing, G Liu - IEEE Transactions on Aerospace and …, 2014 - ieeexplore.ieee.org
… This makes satellite maneuver control much more difficult to implement practically. … in this
paper, a control scheme named six-DOF optimal dynamic inversion control (ODIC) is proposed. …

Guidance and robust generalized inversion based attitude control of satellite launch vehicle

U Ansari, AH Bajodah - … 4th International Conference on Control …, 2016 - ieeexplore.ieee.org
inversion control and its application to attitude control for satellite launch vehicle. In proposed
… For singularity avoidance and stable attitude tracking, a dynamic scale factor is augmented …

Aircraft trajectory tracking by nonlinear spatial inversion

H Bouadi, F Mora-Camino - AIAA Guidance, Navigation, and Control …, 2012 - arc.aiaa.org
… with improved accuracy for spatial trajectory tracking. This should induce increased capacity
… with the hybridization of inertial units with satellite information. However, until today a high …

Generalized dynamic inversion scheme for satellite launch vehicle attitude control

U Ansari, AH Bajodah - IFAC-PapersOnLine, 2015 - Elsevier
inversion attitude control design for satellite launch vehicle. Dynamic constraints that
encapsulate the attitude tracking … and are inverted to solve for the control variables using the …

Adaptive nonlinear dynamic inversion for spacecraft attitude control with fuel sloshing

E Weerdt, EJ Kampen, D Gemert, QP Chu… - … Navigation and Control …, 2008 - arc.aiaa.org
… For Nonlinear Dynamic Inversion controllers, the tracking performance depends on the
model on the plant dynamics. In this paper we explore the response of a controlled satellite with …

Inverse free steering law for small satellite attitude control and power tracking with VSCMGs

MSI Malik, S Asghar - Advances in Space Research, 2014 - Elsevier
inversion, whereas we propose an inverse free steering law. In this paper, H ∞ control
based steering law is designed for VSCMGs performing combined attitude and power tracking. …

Inertia-independent generalized dynamic inversion feedback control of spacecraft attitude maneuvers

AH Bajodah - Acta Astronautica, 2011 - Elsevier
… The generalized dynamic inversion control methodology is applied to the spacecraft attitude
trajectory tracking problem. It is shown that the structure of the skew symmetric cross product …

High precision satellite attitude tracking control via iterative learning control

B Wu, D Wang, EK Poh - Journal of Guidance, Control, and Dynamics, 2015 - arc.aiaa.org
… a satellite with a repeating ground track orbit, in which orbit the satellite can revisit points
along this track … In this section, the attitude control problem for the previously mentioned kind of …

Robust Nonlinear Spacecraft Attitude Control using Incremental Nonlinear Dynamic Inversion.

P Acquatella, W Falkena, EJ van Kampen… - … , Navigation, and Control …, 2012 - arc.aiaa.org
… The most important disturbances for a satellite in orbit are the gravity field of the Earth due to
… First, we demonstrate the Modified Rodrigues Parameters attitude tracking with NDI-control, …

Inverse optimal adaptive control for attitude tracking of spacecraft

W Luo, YC Chu, KV Ling - … Transactions on Automatic Control, 2005 - ieeexplore.ieee.org
… attitude tracking with a global convergence of tracking errors to … ], the adaptive control law
in this paper is inverse optimal with … maneuver control problem of a rigid-body microsatellite is …