Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control

| 7.1 | Given the following system, determine the solution of the homogenous equation (which is normally called either the complementary or transient solution) for the given initial conditions: |
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| 7.2 | Given the following equation for a mass spring damper system where we assume
Given the initial condition, X(0) = 2, find
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| 7.3 | Using the baseline system of Problem 7.2, find the general or total solution if the forcing function is not a constant (that is, step) but of the form with ? = 2 rad/s. |
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| 7.4 | For Problem 7.2 (with the step input) find
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| 7.5 | For the following second-order system and initial conditions, find the transient solution: |
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| 7.6 | Given M = 2, C = 12, K = 50, Y = 2
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| 7.7 | Write out the general solution to Problem 7.6, Part (5), in the phase angle form. |
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| 7.8 | Sketch the time response to... |