Guidance and control of autonomous vehicles is a difficult and often calculation-intensive process. Current control approaches limit the functionality of autonomous vehicles. The approach applied in this thesis is to use a discrete-state model of the vehicle dynamics to build a hybrid automaton. By creating a set of stable trim states and building a library of maneuvers, the on-line optimization problem was made significantly simpler. The implementation of the control methodology for an autonomous helicopter was expanded to include three-dimensional path planning and pilot-inspired maneuvers. The hybrid controller was then adapted and applied to an unpowered parafoil in simulation. The parafoil hybrid controller was also implemented on a DS...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.I...
Designing autonomous flight control system for a mini scale helicopter is very challenging due to th...
Abstract. In this paper we describe the control logic that enabled a small-scale unmanned helicopter...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2001.Includes...
This paper proposes a hierarchical hybrid architecture of a reactive system that governs the operat...
In this paper, the robust hybrid control design is investigated for a small scale helicopter flying ...
This report describes a guidance system for agile vehicles based on a hybrid closed-loop model of th...
In this paper, we propose a hybrid modelling and control design scheme for an unmanned helicopter. T...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
iii Autorotation is a descending maneuver that can be used to recover helicopters in the event of to...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
Dynamics of miniature unmanned helicopter are considered nonlinear and mutually coupled; therefore d...
Autorotation maneuvers are required to perform a safe landing of a helicopter in cases of engine los...
The objective of this work is to develop an autonomous autorotation landing system for an unmanned h...
Around ninety percent of vehicle innovations are driven mainly by electronics. The software implemen...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.I...
Designing autonomous flight control system for a mini scale helicopter is very challenging due to th...
Abstract. In this paper we describe the control logic that enabled a small-scale unmanned helicopter...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2001.Includes...
This paper proposes a hierarchical hybrid architecture of a reactive system that governs the operat...
In this paper, the robust hybrid control design is investigated for a small scale helicopter flying ...
This report describes a guidance system for agile vehicles based on a hybrid closed-loop model of th...
In this paper, we propose a hybrid modelling and control design scheme for an unmanned helicopter. T...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
iii Autorotation is a descending maneuver that can be used to recover helicopters in the event of to...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
Dynamics of miniature unmanned helicopter are considered nonlinear and mutually coupled; therefore d...
Autorotation maneuvers are required to perform a safe landing of a helicopter in cases of engine los...
The objective of this work is to develop an autonomous autorotation landing system for an unmanned h...
Around ninety percent of vehicle innovations are driven mainly by electronics. The software implemen...
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.I...
Designing autonomous flight control system for a mini scale helicopter is very challenging due to th...
Abstract. In this paper we describe the control logic that enabled a small-scale unmanned helicopter...