aircraft:tmd:rigidbody
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- | ==== Rigidbody ===== | + | ===== Rigidbody |
Aerofly uses the mathematical concept of a rigidbody to simulate the aircraft mass. A rigidbody in Aerofly can be thought of as a box with a certain size, a certain mass, position and orientation, | Aerofly uses the mathematical concept of a rigidbody to simulate the aircraft mass. A rigidbody in Aerofly can be thought of as a box with a certain size, a certain mass, position and orientation, | ||
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Allows full 6 degrees of motion: 3 translation components and 3 rotational components. | Allows full 6 degrees of motion: 3 translation components and 3 rotational components. | ||
+ | == Typical short version === | ||
> **Caution**: | > **Caution**: | ||
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+ | == Full version === | ||
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+ | > **Caution**: | ||
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+ | === Rigid == | ||
+ | Setting '' | ||
+ | |||
+ | === R0 === | ||
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+ | '' | ||
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+ | === X0, Y0, Z0 === | ||
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+ | X0, Y0 and Z0 define a rotation matrix to rotate the joint' | ||
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+ | === Kf, Kt == | ||
+ | All '' | ||
+ | '' | ||
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+ | === Df == | ||
+ | All '' | ||
+ | '' | ||
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+ | === ForceMax, TorqueMax === | ||
+ | Defines the force and torque at which the connection breaks. From that moment on the two bodies are completely independant and the crash reset timer is started which reloads the aircraft after (default) 3 seconds. | ||
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+ | === Rotation Input === | ||
+ | |||
+ | Using Rotation0Control, | ||
+ | |||
+ | === PreLoad, PreTension === | ||
+ | Defines the offset force (in Newtons) or torque (in Newton-Meters). When the deflection or displacement is zero this force or torque is still acting between the two bodies. Normally the landing gear would compress under the weight of the aircraft but the PreLoad parameter could reduce this displacement to zero on the ground. In the air the gear would then extend outward. | ||
==== Joint-Torque ==== | ==== Joint-Torque ==== | ||
aircraft/tmd/rigidbody.txt · Last modified: 2018/09/30 14:43 by jh