We present a new quadrotor geometric control scheme that is capable of tracking highly aggressive trajectories. Our geometric controller uses the logarithmic map of SO(3) to express rotational error in the Lie algebra, and we show that it is globally attractive without requiring a complicated hybrid switching scheme. We show the performance of our controller against highly aggressive trajectories in simulation experiments. Additionally, we present an adaptation of this controller that allows us to interface effectively with the angular rate controllers on an onboard flight control unit and show the ability of this adapted control scheme to track aggressive trajectories on a quadrotor hardware platform
In this paper we design a nonlinear controller for aggressive maneuvering of a quadrotor. We take a ...
In this thesis optimal analytical controls derived using the framework of geometric control theory a...
The collocation method is extended to the special orthogonal group SO(3) with application to optimal...
This article proposes a novel integral geometric control attitude tracking scheme, utilizing a coord...
Abstract—This paper provides new results for a robust adaptive tracking control of the attitude dyna...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
This paper introduces an $\mathcal{L}_1$ adaptive control augmentation for geometric tracking contro...
This paper concerns the robustness of attitude controllers for dynamics configured on the SO(3) mani...
The control of a quadrotor is typically split into two subsequent problems: finding desired accelera...
This paper addresses the aggressive formation tracking problem of quadrotors without velocity measur...
\u3cp\u3eThe control of a quadrotor is typically split into two subsequent problems: finding desired...
This paper presents nonlinear tracking control systems for a quadrotor unmanned aerial vehicle under...
Abstract—Nonlinear PID control systems for a quadrotor UAV are proposed to follow an attitude tracki...
none4siIn this paper we design a nonlinear controller for aggressive maneuvering of a quadrotor. We ...
The traditional quadcopter control systems should deal with two common problems. Namely, the singula...
In this paper we design a nonlinear controller for aggressive maneuvering of a quadrotor. We take a ...
In this thesis optimal analytical controls derived using the framework of geometric control theory a...
The collocation method is extended to the special orthogonal group SO(3) with application to optimal...
This article proposes a novel integral geometric control attitude tracking scheme, utilizing a coord...
Abstract—This paper provides new results for a robust adaptive tracking control of the attitude dyna...
Abstract — This paper provides new results for a tracking control of the attitude dynamics of a rigi...
This paper introduces an $\mathcal{L}_1$ adaptive control augmentation for geometric tracking contro...
This paper concerns the robustness of attitude controllers for dynamics configured on the SO(3) mani...
The control of a quadrotor is typically split into two subsequent problems: finding desired accelera...
This paper addresses the aggressive formation tracking problem of quadrotors without velocity measur...
\u3cp\u3eThe control of a quadrotor is typically split into two subsequent problems: finding desired...
This paper presents nonlinear tracking control systems for a quadrotor unmanned aerial vehicle under...
Abstract—Nonlinear PID control systems for a quadrotor UAV are proposed to follow an attitude tracki...
none4siIn this paper we design a nonlinear controller for aggressive maneuvering of a quadrotor. We ...
The traditional quadcopter control systems should deal with two common problems. Namely, the singula...
In this paper we design a nonlinear controller for aggressive maneuvering of a quadrotor. We take a ...
In this thesis optimal analytical controls derived using the framework of geometric control theory a...
The collocation method is extended to the special orthogonal group SO(3) with application to optimal...