Add to ORKGThe nonlinear set of equations which represent helicopter motion is linearized about a prescribed nominal state. Once the linearized system is obtained it is validated by comparing the output of the nonlinear system to that of its linearized counterpart. Having obtained a linear model, linear system theory may then be applied in order to investigate the stability and control characteristics of the aircraft
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
Modeling, Control and Coordination of Helicopter Systems provides a comprehensive treatment of helic...
The nonlinear set of equations which represents helicopter motion are linearized about a prescribed ...
Developing mathematical model for tandem rotor helicopter for analysis of automatic approach and lan...
In this paper, output tracking control of a helicopter model is investigated. The model is derived f...
In this paper, output tracking control of a helicopter model is investigated. The model is derived f...
Helicopter modeling is a complex task as helicopters consist of many subsystems (nacelle, rotor, eng...
Nonlinear control methods are difficult to work on an unmanned helicopter system for its inherently ...
A set of linearized equations of motion to predict the linearized dynamic response of a single rotor...
This paper presents an adaptive feedback linearization approach to derive helicopter. Ideal feedback...
The helicopter is specific in regards to other traffictransportation means, not just by its structur...
SIGLEAvailable from British Library Document Supply Centre-DSC:DX192472 / BLDSC - British Library Do...
The paper focuses on the fundamental challenge of generating linear equivalent systems and accurate ...
The validation of theoretical flight-mechanics models for helicopters is of considerable practical i...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
Modeling, Control and Coordination of Helicopter Systems provides a comprehensive treatment of helic...
The nonlinear set of equations which represents helicopter motion are linearized about a prescribed ...
Developing mathematical model for tandem rotor helicopter for analysis of automatic approach and lan...
In this paper, output tracking control of a helicopter model is investigated. The model is derived f...
In this paper, output tracking control of a helicopter model is investigated. The model is derived f...
Helicopter modeling is a complex task as helicopters consist of many subsystems (nacelle, rotor, eng...
Nonlinear control methods are difficult to work on an unmanned helicopter system for its inherently ...
A set of linearized equations of motion to predict the linearized dynamic response of a single rotor...
This paper presents an adaptive feedback linearization approach to derive helicopter. Ideal feedback...
The helicopter is specific in regards to other traffictransportation means, not just by its structur...
SIGLEAvailable from British Library Document Supply Centre-DSC:DX192472 / BLDSC - British Library Do...
The paper focuses on the fundamental challenge of generating linear equivalent systems and accurate ...
The validation of theoretical flight-mechanics models for helicopters is of considerable practical i...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
Modeling, Control and Coordination of Helicopter Systems provides a comprehensive treatment of helic...