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Dias nummer 1

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To describe the motion of the helicopter (frame) generated by forces and torques ... No cross-coupling because of teetering rotor (no hinge-offset) ... – PowerPoint PPT presentation

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Title: Dias nummer 1


1
Modelling of Helicopter
Next Presenter Ulrik
Topic Modelling of the Helicopter
Ulrik
2
Motion of Rigid Body
Purpose of Block
  • To describe the motion of the helicopter (frame)
    generated by forces and torques

Output Motion-parameters
  • V the translatory velocity-vector
  • w the angular velocity-vector
  • (Q) the Euler-angles (used as feedback to
    Forces and Torques Block)
  • (P) the position of the helicopter (used as
    input to VR model)

Ulrik
3
Motion of Rigid Body
1st Objective
  • Relate vector-description in BF to its
    description in SF

Direction Cosine by 3-2-1 Euler angle rotation
Thus, a vector x stated in BF is stated in SF as
Ulrik
4
Motion of Rigid Body
2nd Objective
  • Rotational motion of the helicopter

Angular Acceleration
External torque-vector
Angular momentum
Angular acceleration-vector
Ulrik
5
Motion of Rigid Body
3rd Objective
  • Translatory motion of the helicopter

Translatory Acceleration
Translatory acceleration originating from
rotation created by w
Translatory acceleration not originating from
rotation created by w
Ulrik
6
Generation of Forces and Torques
Purpose of Block
  • To describe forces and torques leading to the
    motion of the helicopter

Output Parameters
  • F the resultant force-vector acting on the
    helicopter
  • t the resultant torque-vector acting on the
    helicopter

Ulrik
7
Generation of Forces and Torques
1st Objective
  • The derivation of the forces acting on the
    helicopter

Origin of Forces
  • bFMR Force generated by main rotor
  • bFTR Force generated by tail rotor
  • bFg The gravitational force

The Resultant Force-Vector
Ulrik
8
Generation of Forces and Torques
Force Generated by Main Rotor
The resultant force-vector
Ulrik
9
Generation of Forces and Torques
Force Generated by Tail Rotor
The resultant force-vector
Gravitational Force
Ulrik
10
Generation of Forces and Torques
2nd Objective
  • The derivation of the torques acting on the
    helicopter

Origin of Torques
  • btMR Torque caused by main rotor
  • btTR Torque caused by tail rotor
  • btD Counter-torque caused by drag on main rotor
  • (Torque caused by tail-rotor drag)

The Resultant Torque-Vector
Ulrik
11
Generation of Forces and Torques
Torque Caused by Main Rotor
Resultant torque-vector
Ulrik
12
Generation of Forces and Torques
Torque Caused by Tail Rotor
Resultant torque-vector
Ulrik
13
Generation of Forces and Torques
Counter-Torque Caused by Drag on the Main Rotor
Simple model Koo et al
Resultant torque-vector
Ulrik
14
Generation of Flapping and Thrust
Purpose of Block
  • To describe aerodynamic relations that yield
    thrust and flapping angles, when control inputs
    are applied.

Output Parameters
  • TMR Thrust generated by main rotor
  • TTR Thrust generated by tail rotor
  • b1s Lateral flapping angle
  • b1c Longitudinal flapping angle

Ulrik
15
Generation of Flapping and Thrust
1st Objective
  • Describe the thrust-generation process.

Thrust Generated By Main Rotor
Ulrik
16
Generation of Flapping and Thrust
Thrust Generated by Tail Rotor
  • Purpose is to compensate for the resultant
    torque about bz (bN)
  • This is assumed done by an onboard
    yaw-controller, so bN0

Thus
..becomes
  • uped is inserted such that it is possible to
    perform a yaw movement

Ulrik
17
Generation of Flapping and Thrust
2nd Objective
  • Describe the flapping angles

Mixer System
Ulrik
18
Generation of Flapping and Thrust
Control-Rotor Flapping equations Mustafic et al
  • Cross-Coupling is present

Mixer System
Ulrik
19
Generation of Flapping and Thrust
Main-Rotor Flapping equations Mustafic et al
  • No cross-coupling because of teetering rotor (no
    hinge-offset)

Ulrik
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