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Helicopter Flight Dynamics
Unit 5: Helicopter Flight Controllers
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Topics External forces acting on helicopter
Control manners of helicopter Control systems and their mechanical characteristic The Development of helicopter controllers
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External Forces Acting on Helicopter
V
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Aerodynamic Forces of Main Rotor
Thrust: T Hind force: H Side force: S Anti-torque: Mk Hub moments: MGx, MGz
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Aerodynamic Forces of Tail Rotor
V Thrust: TT Anti-torque: MkT
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Aerodynamic Forces of Fuselage
Drag: Qf Lift: Yf Side Force: Sf Roll Moment: Mxf Yaw Moment: Myf Pitch Moment: Mzf V
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Aerodynamic Forces of Horizontal Tail
V Drag: Dh Lift: Yh
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Aerodynamic Forces of Vertical Tail
Drag: Dv Lift: Yv
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Helicopter Control Manners
Control manners of helicopter with main rotor and tail rotor Control manners of twin rotors helicopter Control manners of tilt-rotor aircraft Other control manners
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Helicopter Types
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Control of Fixed-wing Aircraft
rudder elevator aileron aileron
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Control of Fixed-wing Aircraft
Degree of Freedoms Cockpit Control Unit Aerodynamic Surfaces Control Forces Direct Control Forward Throttle Thrust T Pitch Stick Elevator MZ Roll Aileron MX Yaw Paddle Rudder MY Indirect Control Altitude Stick + Throttle F Sideward Stick + Paddle S
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Control of Helicopter Main Rotor Control System Engines Tail Rotor
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Control of Helicopter with Main & Tail Rotors
Degree of Freedoms Motions Cockpit Control Unit Aerodynamic Surfaces Control Forces Vertical Altitude Collective stick Rotor T Longitudinal Pitching, Forward & backward Stick H, MGz Lateral Rolling, sidestep S, MGx Yaw Heading Rudder Tail rotor TT Main rotor is the lift surface to produce the lift of helicopter. On the other hand, it is the control surface to produce the forces or moments of heaving, pitching and rolling. Furthermore, it is the propeller to make helicopter to fly in any directions.
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Comparison of Control Between helicopter and Fixed-wing Aircraft
Degree of Freedoms Cockpit Control Unit Aerodynamic Surfaces Control Forces Helicopter Direct Control Altitude Collective Rotor T Pitch Stick H, MGz Roll S, MGx Yaw Rudder Tail rotor TT Indirect Control Forward Collective + stick H Sideward Collective + stick + Rudder S Fixed_wing Aircraft Throttle Thrust Elevator MZ Aileron MX Paddle MY Stick + Throttle F Stick + Paddle
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Control of Tilt-rotor Aircraft
Airplane Helicopter Thrust /power level controls Collective pitch and throttles Acts as altitude control Thrust /power level controls blade pitch and engine throttles Acts as altitude control Thrust/power Control
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Control of Tilt-rotor Aircraft
Helicopter Airplane Forward longitudinal cyclic pitch elevator Proprotor discs tilt forward Aircraft assumes nose-down altitude Airspeed increases Elevator deflects downward Altitude decreases Forward Stick Control
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Control of Tilt-rotor Aircraft
Helicopter Airplane elevator Backward longitudinal cyclic pitch Proprotor discs tilt backward Aircraft assumes nose-up altitude Airspeed decreases Elevator deflects upward Altitude increases Backward Stick Control
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Control of Tilt-rotor Aircraft
Helicopter Airplane differential collective pitch and lateral cyclic pitch flaperon Right proprotor increase collective pitch Left proprotor decrease collective pitch Proprotor discs tilt to left Aircraft rolls to left Right flaperon deflects downward Left flaperon deflects downward Left Stick Control
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Control of Tilt-rotor Aircraft
Helicopter Airplane differential collective pitch and lateral cyclic pitch flaperon Left proprotor increase collective pitch Right proprotor decrease collective pitch Proprotor discs tilt to right Aircraft rolls to right Left flaperon deflects downward Right flaperon deflects downward Right Stick Control
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Control of Tilt-rotor Aircraft
Helicopter Airplane Differential longitudinal cyclic Rudder Left proprotor disk tilts forward Right proprotor disk tilts backward Aircraft yaws to left Rudder deflect to left Left Pedal Control
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Control of Tilt-rotor Aircraft
Helicopter Airplane Differential longitudinal cyclic Rudder Left proprotor disk tilts backward Right proprotor disk tilts forward Aircraft yaws to right Rudder deflect to right Right Pedal Control
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The Development of Controller
Smart Control System Ambient disturbance Information from navigation sys. Commands from pilot Airborne Computer Helicopter flight dynamic model Actuators Sensors Helicopter
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