This paper presents a novel control algorithm for tracking of nonlinear dynamic systems. The tracking problem leads to linearized time-varying error equations. Hence new eigenvalue notions are introduced for linear time varying systems, and a PD eigenstructure assignment scheme is proposed for linear time-varying structure via a differential Sylvester equation. Also shown is that closed-loop systems could be stabilized by assigning PD-eigenvalues appropriately, and a desired performance could be obtained by assigning the PD-eigenvectors according to the design specifications. The present control algorithm has an internal framework for testing the controllability of the time varying system via Lyapunov transform. The algorithm proposed is ve...
This paper presents a novel adaptive control algorithm solving the trajectory tracking problem for q...
This paper presents a novel adaptive control algorithm solving the trajectory tracking problem for q...
The dynamic response characteristics of modern unmanned aerial vehicles (UAVs) are highly nonlinear ...
This paper presents a novel control algorithm for tracking of nonlinear dynamic systems. The trackin...
This paper develops a trajectory tracking control design algorithm to be applied in unmanned aerial ...
A nonlinear optimal control approach is developed for the UAV and suspended load system. The dynamic...
Abstract—An output feedback (OFB) dynamic inversion control strategy is developed for an unmanned ae...
This paper presents the linear quadratic tracking (LQT) control of a quadrotor UAV by solving discre...
This paper presents a novel configuration for guidance and tracking control laws for unmanned air ve...
This paper presents a complete trajectory tracking controller design for an Unmanned Air Vehicle usi...
This paper presents a complete trajectory tracking controller design for an Unmanned Air Vehicle usi...
This paper presents a novel configuration for guidance and tracking control laws for unmanned air ve...
This paper presents a complete trajectory tracking controller design for an Unmanned Air Vehicle usi...
To facilitate accurate tracking in unknown/uncertain environments, this paper proposes a simple lear...
In this thesis a new linear parameter-varying sliding mode control (LPVSMC) approach is developed fo...
This paper presents a novel adaptive control algorithm solving the trajectory tracking problem for q...
This paper presents a novel adaptive control algorithm solving the trajectory tracking problem for q...
The dynamic response characteristics of modern unmanned aerial vehicles (UAVs) are highly nonlinear ...
This paper presents a novel control algorithm for tracking of nonlinear dynamic systems. The trackin...
This paper develops a trajectory tracking control design algorithm to be applied in unmanned aerial ...
A nonlinear optimal control approach is developed for the UAV and suspended load system. The dynamic...
Abstract—An output feedback (OFB) dynamic inversion control strategy is developed for an unmanned ae...
This paper presents the linear quadratic tracking (LQT) control of a quadrotor UAV by solving discre...
This paper presents a novel configuration for guidance and tracking control laws for unmanned air ve...
This paper presents a complete trajectory tracking controller design for an Unmanned Air Vehicle usi...
This paper presents a complete trajectory tracking controller design for an Unmanned Air Vehicle usi...
This paper presents a novel configuration for guidance and tracking control laws for unmanned air ve...
This paper presents a complete trajectory tracking controller design for an Unmanned Air Vehicle usi...
To facilitate accurate tracking in unknown/uncertain environments, this paper proposes a simple lear...
In this thesis a new linear parameter-varying sliding mode control (LPVSMC) approach is developed fo...
This paper presents a novel adaptive control algorithm solving the trajectory tracking problem for q...
This paper presents a novel adaptive control algorithm solving the trajectory tracking problem for q...
The dynamic response characteristics of modern unmanned aerial vehicles (UAVs) are highly nonlinear ...