Abstract
The main objective of this paper is to give a basic understanding of the mechanisms through which pilot cyclic inputs in lateral cyclic interacts with high-order rotor dynamics destabilizing the helicopter roll motion. The paper will use a “Newtonian formulation” representing the main forces acting on the airframe body-rotor system as the pilot applies his/her control. It will be demonstrated that pilot lateral controls applied through his/her arm (which may involve also pilot biodynamics, i.e. the dynamics of pilot neuromuscular inputs and contraction dynamics of his/her muscles) may excite much higher-order frequency rotor dynamics than thought at the present.
Original language | English |
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Pages (from-to) | 139-156 |
Number of pages | 18 |
Journal | INCAS Bulletin |
Volume | 10 |
Issue number | 3 |
DOIs | |
Publication status | Published - 2018 |
Event | 6th CEAS Air and Space Conference - Palace of the Parliament, Bucharest, Romania Duration: 16 Oct 2017 → 20 Oct 2017 Conference number: 6 http://ceas2017.org/ |
Keywords
- Helicopter
- Pilot Assisted Oscillations
- Rotorcraft Pilot Couplings
- Lead-lag mode
- Rotor dynamics