Flight Dynamics II
£3.25
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Flight Dynamics II
£3.25
Part 2 of 2 in the Flight Dynamics series. Topics in this product include trim conditions, stability derivatives, longitudinal and lateral stability (the Phugoid, roll subsidence, spiral and Dutch roll modes), and control derivatives with PID tuning.
This is a 10-page PDF scan of handwritten notes, featuring clickable PDF bookmarks so you can jump straight to any page in a PDF viewer such as Adobe Acrobat. Complete page-by-page contents can be found below so you know exactly what's inside before you buy.
ControlsPage-by-page contents
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Page-by-page contents
- 01Aircraft state equations, euler angles, matrix form, singular point, augmented inertia matrix, jacobian
- 02Trim conditions, equilibrium, trim equation, linearisation, Curie principle
- 03Stability derivatives, U-derivatives
- 04W-derivatives, q-derivatives, W dot derivatives
- 05State space structure, eigenvalues, longitudinal stability quartic, lateral stability quintic, Routh's discriminant
- 06Root-locus diagram, longitudinal stability quartic
- 07Small quadratic, Phugoid mode, lateral stability quintic, roll subsidence, spiral mode, dutch roll
- 08Control inputs, control derivatives, longitudinal and lateral control derivatives, transfer functions
- 09Roll response to aileron step input, pitch rate response to step elevator input, PID control
- 10Tuning PID gains