A flight investigation was conducted to determine the characteristic shapes of the altitude, ground speed, and deceleration profiles of visual approaches for helicopters. Two hundred thirty-six visual approaches were flown from nine sets of initial conditions with four types of helicopters. Mathematical relationships were developed that describe the characteristic visual deceleration profiles. These mathematical relationships were expanded to develop equations which define the corresponding nominal ground speed, pitch attitude, pitch rate, and pitch acceleration profiles. Results are applicable to improved helicopter handling qualities in terminal area operations
A ground-simulation experiment was conducted to investigate the influence and interaction of flight-...
A helicopter height velocity (HV) diagram was analytically constructed using optimal control techniq...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
Control-display requirements for helicopters conducting decelerating approaches in the terminal area...
The studies were undertaken to investigate the effects of rotor design parameters, interaxis couplin...
A flight investigation was undertaken to study the problems associated with manual and automatic con...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
The results of a survey of the flight conditions experienced by three military helicopters engaged i...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
A survey of commercial helicopter-operating experiences was conducted using a helicopter flight reco...
Helicopters are used by the military and civilian communities for a variety of tasks and must be cap...
Helicopter height-velocity diagram analysis showing effects of density altitude and gross weigh
Military helicopter operations require precise maneuverability characteristics for performance to be...
A helicopter height velocity (HV) diagram was analytically constructed using optimal control techniq...
A ground-simulation experiment was conducted to investigate the influence and interaction of flight-...
A helicopter height velocity (HV) diagram was analytically constructed using optimal control techniq...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...
Control-display requirements for helicopters conducting decelerating approaches in the terminal area...
The studies were undertaken to investigate the effects of rotor design parameters, interaxis couplin...
A flight investigation was undertaken to study the problems associated with manual and automatic con...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
The results of a survey of the flight conditions experienced by three military helicopters engaged i...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
A survey of commercial helicopter-operating experiences was conducted using a helicopter flight reco...
Helicopters are used by the military and civilian communities for a variety of tasks and must be cap...
Helicopter height-velocity diagram analysis showing effects of density altitude and gross weigh
Military helicopter operations require precise maneuverability characteristics for performance to be...
A helicopter height velocity (HV) diagram was analytically constructed using optimal control techniq...
A ground-simulation experiment was conducted to investigate the influence and interaction of flight-...
A helicopter height velocity (HV) diagram was analytically constructed using optimal control techniq...
An investigation was made in the Langley V/STOL tunnel to determine rotor induced effects on a 1/4-s...