The main purpose of this paper is to develop an onboard adaptive and robust flight control system that improves control, stability, and survivability of a small unmanned aerial system in off-nominal or out-of-envelope conditions. The aerodynamics of aircraft associated with hazardous and adverse onboard conditions is inherently nonlinear and unsteady. The presented flight control system improves functionalities required to adapt the flight control in the presence of aircraft model uncertainties. The fault tolerant inner loop is enhanced by an adaptive real-time artificial neural network parameter identification to monitor important changes in the aircraft’s dynamics due to nonlinear and unsteady aerodynamics. The real-time artificial neural...
The control of systems with uncertain nonlinear dynamics is an important field of control science at...
This dissertation presents the design, development, and simulation testing of an adaptive trajectory...
In this paper, Levenberg–Marquardt inspired sliding mode control theory based adaptation laws are pr...
The main purpose of this paper is to develop an onboard adaptive and robust flight control system th...
A reconfigurable flight control method is developed to be implemented on an Unmanned Aircraft (UA), ...
The nonlinear and unsteady nature of aircraft aerodynamics together with limited practical range of ...
With the increasing demand for unmanned aerial vehicles (UAVs) in both military and civilian applica...
A dissertation submitted to the Faculty of Engineering and the Built Environment, University of the...
This article proposes an adaptive flight framework that integrates a discrete-time incremental nonli...
An innovative neuro-adaptive design philosophy is presented in this paper embedding a Sobolev norm b...
The paper deals with the stabilisation and trajectory tracking control of an autonomous quadrotor he...
This thesis presents the development of small, inexpensive unmanned aerial vehicles (UAVs) to achie...
For the ultralow altitude airdrop decline stage, many factors such as actuator nonlinearity, the un...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2010.This e...
Stabilizing the Unmanned Aircraft Systems (UAS) under complex environment including system uncertain...
The control of systems with uncertain nonlinear dynamics is an important field of control science at...
This dissertation presents the design, development, and simulation testing of an adaptive trajectory...
In this paper, Levenberg–Marquardt inspired sliding mode control theory based adaptation laws are pr...
The main purpose of this paper is to develop an onboard adaptive and robust flight control system th...
A reconfigurable flight control method is developed to be implemented on an Unmanned Aircraft (UA), ...
The nonlinear and unsteady nature of aircraft aerodynamics together with limited practical range of ...
With the increasing demand for unmanned aerial vehicles (UAVs) in both military and civilian applica...
A dissertation submitted to the Faculty of Engineering and the Built Environment, University of the...
This article proposes an adaptive flight framework that integrates a discrete-time incremental nonli...
An innovative neuro-adaptive design philosophy is presented in this paper embedding a Sobolev norm b...
The paper deals with the stabilisation and trajectory tracking control of an autonomous quadrotor he...
This thesis presents the development of small, inexpensive unmanned aerial vehicles (UAVs) to achie...
For the ultralow altitude airdrop decline stage, many factors such as actuator nonlinearity, the un...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2010.This e...
Stabilizing the Unmanned Aircraft Systems (UAS) under complex environment including system uncertain...
The control of systems with uncertain nonlinear dynamics is an important field of control science at...
This dissertation presents the design, development, and simulation testing of an adaptive trajectory...
In this paper, Levenberg–Marquardt inspired sliding mode control theory based adaptation laws are pr...