flight control

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Last updated 12:33 AM on 5/23/26
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4 Terms

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<p>2nd order short period dynamic mode approximation</p>

2nd order short period dynamic mode approximation

  • in short period approximations, we assumed one degree of freedom (pitch rotation), but a real aircraft is rotating and translating in 6 total degrees of freedom. we need a static reference frame to describe these motions - most commonly a catersian earth coordinate system

<ul><li><p>in short period approximations, we assumed one degree of freedom (pitch rotation), but a real aircraft is rotating and translating in 6 total degrees of freedom. we need a static reference frame to describe these motions - most commonly a catersian earth coordinate system </p></li></ul><p></p>
2
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<p>lomgitudinal equations of motion </p>

lomgitudinal equations of motion

assumptions

  • L normal to V

  • drag parrallel and opposite to V

  • thrust acts along V

  • summing all forces around CG

<p>assumptions </p><ul><li><p>L normal to V</p></li><li><p>drag parrallel and opposite to V</p></li><li><p>thrust acts along V</p></li><li><p>summing all forces around CG</p></li></ul><p></p>
3
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complex planes (eigen values)

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