Add to ORKGA brief summary is made of methods available to the helicopter designer for obtaining desired stability characteristics by modifications to the airframe design. The discussion is based on modifications made during the establishment of flying-qualities criteria and includes sample indications of theoretical studies of additional methods
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
The stability and control of rotors at high advance ratio are considered. Teetering, articulated, gi...
In thefirst part of thk report a brief review ti presded of methodsavailableto the helicopterdm”grwr...
Part I of this report presents a brief review of methods available to the helicopter designer for ob...
In order to provide engineers interested in rotating-wing aircraft, but with no specialized training...
Maneuver stability characteristics of tandem rotor transport helicopter determined by flight test - ...
The studies were undertaken to investigate the effects of rotor design parameters, interaxis couplin...
This report outlines the flight conditions that are usually critical in determining the design of co...
Joint NASA/Army efforts at the Ames Research Center to develop rotorcraft handling-qualities design ...
The analytical capability of the helicopter stability program is discussed. The parameters which are...
A sequence of ground and flight simulation experiments was conducted to investigate helicopter instr...
A theoretical analysis of helicopter maneuver stability is made and the results are compared with ex...
Helicopters are used by the military and civilian communities for a variety of tasks and must be cap...
A brief summary is made of methods available to the helicopter designer for obtaining desired stabil...
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
The stability and control of rotors at high advance ratio are considered. Teetering, articulated, gi...
In thefirst part of thk report a brief review ti presded of methodsavailableto the helicopterdm”grwr...
Part I of this report presents a brief review of methods available to the helicopter designer for ob...
In order to provide engineers interested in rotating-wing aircraft, but with no specialized training...
Maneuver stability characteristics of tandem rotor transport helicopter determined by flight test - ...
The studies were undertaken to investigate the effects of rotor design parameters, interaxis couplin...
This report outlines the flight conditions that are usually critical in determining the design of co...
Joint NASA/Army efforts at the Ames Research Center to develop rotorcraft handling-qualities design ...
The analytical capability of the helicopter stability program is discussed. The parameters which are...
A sequence of ground and flight simulation experiments was conducted to investigate helicopter instr...
A theoretical analysis of helicopter maneuver stability is made and the results are compared with ex...
Helicopters are used by the military and civilian communities for a variety of tasks and must be cap...
A brief summary is made of methods available to the helicopter designer for obtaining desired stabil...
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
The stability and control of rotors at high advance ratio are considered. Teetering, articulated, gi...