Approaches for a tether-guided landing of an autonomous helicopter
- 5 June 2006
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Robotics
- Vol. 22 (3) , 536-544
- https://doi.org/10.1109/tro.2006.870657
Abstract
In this paper, we address the design of an autopilot for autonomous landing of a helicopter on a rocking ship, due to rough sea. A tether is used for landing and securing a helicopter to the deck of the ship in rough weather. A detailed nonlinear dynamic model for the helicopter is used. This model is underactuated, where the rotational motion couples into the translation. This property is used to design controllers which separate the time scales of rotation and translation. It is shown that the tether tension can be used to couple the translation of the helicopter to the rotation. Two controllers are proposed in this paper. In the first, the rotation time scale is chosen much shorter than the translation, and the rotation reference signals are created to achieve a desired controlled behavior of the translation. In the second, due to coupling of the translation of the helicopter to the rotation through the tether, the translation reference rates are created to achieve a desired controlled behavior of the attitude and altitude. Controller A is proposed for use when the helicopter is far away from the goal, while Controller B is for the case when the helicopter is close to the ship. The proposed control schemes are proved to be robust to the tracking error of its internal loop and results in local exponential stability. The performance of the control system is demonstrated by computer simulations. Currently, work is in progress to implement the algorithm using an instrumented model of a helicopter with a tether.Keywords
This publication has 22 references indexed in Scilit:
- Equilibrium-to-Equilibrium Maneuvers of Flexible Electrodynamic Tethers in Equatorial OrbitsJournal of Spacecraft and Rockets, 2006
- (Almost) exact path tracking control for an autonomous helicopter in hover manoeuvresPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Trajectory tracking control design for autonomous helicopters using a backstepping algorithmPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2000
- Technical Note: Robust Multivariable Control of Rotorcraft in Forward Flight: Impact of Bandwidth on Fatigue LifeJournal of the American Helicopter Society, 1998
- Helicopter Attitude Command Attitude Hold Using Individual Channel Analysis and DesignJournal of Guidance, Control, and Dynamics, 1997
- Robust Longitudinal Control Design Using Dynamic Inversion and Quantitative Feedback TheoryJournal of Guidance, Control, and Dynamics, 1997
- Behaviour-based control: examples from navigation, learning, and group behaviourJournal of Experimental & Theoretical Artificial Intelligence, 1997
- Synthesis and evaluation of an H2 control law for a hovering helicopterJournal of Guidance, Control, and Dynamics, 1993
- Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraftAutomatica, 1992
- Synthesis of a helicopter full-authority controllerJournal of Guidance, Control, and Dynamics, 1992