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If applied: This commit on top of the current forceCoeffs allows the user to compute:
- Side force coefficient whose direction in curl(lift,drag),
- Yaw moment coefficient whose rotation axis in dir(lift),
- Roll moment coefficient whose rotation axis in dir(drag)
- Also, for developers:
- Destructor is = default
- Some divisions were replaced by multiplications
- Some repetitive multiplications were reduced to a single oper
- Name change: momentCoeff -> pitchMomentCoeff
- Order of output is reorganised as moments(pitch,yaw,roll) and forces(lift,drag,side)
- For force coefs, the front and rear axles' contributions are computed
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Verification: Passed sanity checks and valgrind-memcheck
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What's next:
- Update for the Extended code guide entry
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Related:
- Designated pitch, yaw, roll orientation can be seen in: en.wikipedia.org/wiki/Yaw_(rotation)#/media/File:Flight_dynamics_with_text.png