Several types of rotors which employ multicyclic control are reviewed and compared. Their differences are high-lighted and their potential advantages and disadvantages are discussed. The flow field these rotors must operate in is discussed, and it is shown that simultaneous elimination of vibration and oscillatory blade loads is not an inherent solution to the roughness problem. The use of rotor blades as energy absorbers is proposed. Input-output relations are considered and a gain control for ROMULAN, a multicyclic controlling computer program, is introduced. Implications of the introduction of multicyclic systems into helicopters are discussed
A class of algorithms for the multicyclic control of helicopter vibration and loads is derived and d...
A control method is proposed to reduce vibrations in helicopters using active trailing-edge flaps on...
Helicopters encounter several constraints such as high vibration and noise levels, and relatively hi...
Results of an investigation into methods of controller design for an individual helicopter rotor bla...
Results of wind tunnel tests of a 12 meter-diameter-rotor utilizing multicyclic jet-flap control def...
The feasibility of automatically providing higher harmonic control to a deflectable control flap at ...
In 2007, the helicopter community celebrated 100 years of helicopter flight. Although no photos or f...
A new, advanced system for active control of helicopters and its application to the solution of roto...
Higher harmonic blade feathering for helicopter vibration reduction is considered. Recent wind tunne...
Since the early helicopter developments, these aircraft have made a tremendous progress in performan...
A type of active control for helicopters was designed and tested on a four foot diameter model rotor...
Modern helicopters still suffer from many problems that hinder a further increase in their efficienc...
The equations of motion are derived for a multiblade rotor. A high twist capability and coupled flat...
This paper describes the DLR’s patented multiple swashplate control system (META) as a new means of ...
Since the early helicopter developments, these aircraft have made a tremendous progress in performan...
A class of algorithms for the multicyclic control of helicopter vibration and loads is derived and d...
A control method is proposed to reduce vibrations in helicopters using active trailing-edge flaps on...
Helicopters encounter several constraints such as high vibration and noise levels, and relatively hi...
Results of an investigation into methods of controller design for an individual helicopter rotor bla...
Results of wind tunnel tests of a 12 meter-diameter-rotor utilizing multicyclic jet-flap control def...
The feasibility of automatically providing higher harmonic control to a deflectable control flap at ...
In 2007, the helicopter community celebrated 100 years of helicopter flight. Although no photos or f...
A new, advanced system for active control of helicopters and its application to the solution of roto...
Higher harmonic blade feathering for helicopter vibration reduction is considered. Recent wind tunne...
Since the early helicopter developments, these aircraft have made a tremendous progress in performan...
A type of active control for helicopters was designed and tested on a four foot diameter model rotor...
Modern helicopters still suffer from many problems that hinder a further increase in their efficienc...
The equations of motion are derived for a multiblade rotor. A high twist capability and coupled flat...
This paper describes the DLR’s patented multiple swashplate control system (META) as a new means of ...
Since the early helicopter developments, these aircraft have made a tremendous progress in performan...
A class of algorithms for the multicyclic control of helicopter vibration and loads is derived and d...
A control method is proposed to reduce vibrations in helicopters using active trailing-edge flaps on...
Helicopters encounter several constraints such as high vibration and noise levels, and relatively hi...