Add to ORKGMethods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The paper describes a method for guiding a dynamic system through a given set of points. The paradig...
This thesis presents the flight trajectory analysis for a given aircraft configuration starting wit...
The nonlinear set of equations which represent helicopter motion is linearized about a prescribed no...
The nonlinear set of equations which represents helicopter motion are linearized about a prescribed ...
A set of linearized equations of motion to predict the linearized dynamic response of a single rotor...
A mathematical model of an advanced helicopter is described. The model is suitable for use in contro...
A mathematical model, suitable for piloted simulation of the flying qualities of helicopters, is a n...
The governing equations of motion of a helicopter rotor coupled to a rigid body fuselage are derived...
This paper outlines the development of a mathematical model that is expected to be useful for rotorc...
Using automatic control theory with simple pilot model for synthesizing helicopter landing approach ...
A mathematical model suitable for real time simulation of the CH-53 helicopter is presented. This mo...
A technique is described for determining the trims and quasi-static derivatives of a flight vehicle ...
A linearized model of rotorcraft dynamics has been developed through the use of symbolic automatic e...
A study on the kinematic relationship of the variables of helicopter motion in steady, coordinated t...
Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The paper describes a method for guiding a dynamic system through a given set of points. The paradig...
This thesis presents the flight trajectory analysis for a given aircraft configuration starting wit...
The nonlinear set of equations which represent helicopter motion is linearized about a prescribed no...
The nonlinear set of equations which represents helicopter motion are linearized about a prescribed ...
A set of linearized equations of motion to predict the linearized dynamic response of a single rotor...
A mathematical model of an advanced helicopter is described. The model is suitable for use in contro...
A mathematical model, suitable for piloted simulation of the flying qualities of helicopters, is a n...
The governing equations of motion of a helicopter rotor coupled to a rigid body fuselage are derived...
This paper outlines the development of a mathematical model that is expected to be useful for rotorc...
Using automatic control theory with simple pilot model for synthesizing helicopter landing approach ...
A mathematical model suitable for real time simulation of the CH-53 helicopter is presented. This mo...
A technique is described for determining the trims and quasi-static derivatives of a flight vehicle ...
A linearized model of rotorcraft dynamics has been developed through the use of symbolic automatic e...
A study on the kinematic relationship of the variables of helicopter motion in steady, coordinated t...
Methods of automatically controlling the airplane are reviewed. Equations for the controlled motion ...
The paper describes a method for guiding a dynamic system through a given set of points. The paradig...
This thesis presents the flight trajectory analysis for a given aircraft configuration starting wit...