Mech 215 Flashcards

1
Q

Newton’s 2nd law in a non-inertial frame

A

∑Fext + Ffict = ma, where Ffict is the fictitious force, and a is the acceleration of the mass within the moving frame.

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2
Q

Ffict

A

-ma, where a is the acceleration of the moving frame.

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3
Q

Damping ratio > 1

A

Amplification

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4
Q

Damping ratio < 1

A

Mitigation

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5
Q

Phase shift < 0

A

Output delayed

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6
Q

Phase shift > 0

A

Output in advance

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7
Q

Harmonic forced response

A

Output is always delayed and mitigated with respect to the input.

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8
Q

When does resonance occur?

A

When the system is excited at the resonance frequency.

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9
Q

Requirement of frequency analysis

A

All initial conditions are set to zero.

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10
Q

Output delay of a first order system

A

Phase shift of the FRF/ input frequency

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11
Q

Output amplitude of a first order system

A

alphamodulus(FRF), where alpha is the coefficient of the harmonic input.

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12
Q

Bode plot positive gain

A

Amplification of the harmonic forced response.

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13
Q

Bode plot negative gain

A

Mitigation of the harmonic forced response.

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14
Q

If T(s) = T1(s)T2(s), then then gain and phase are (respectively)…

A

gain1(w) + gain2(w) and phiH1 + phiH2

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15
Q

If T(s) = T1(s)/T2(s), then then gain and phase are (respectively)…

A

gain1(w) - gain2(w) and phiH1 - phiH2

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16
Q

Bode stability criterion

A

A system is stable if the open loop gain is negative at the critical frequency, wc.

17
Q

Critical frequency, wc

A

The frequency when the phase is -π.

18
Q

Gain margin

A

GM = -Gain(wc). This corresponds to the gain that can be added to the system whilst preserving its stability.

19
Q

Phase margin

A

PM = π + phase(wgo), where wgo is the frequency at zero gain. This corresponds to the phase delay that can be added to a system whilst preserving its stability.

20
Q

Steady state error, ess

A

lim(s->0)(SU(s)/1 + T1(s)T2(s))

21
Q

What does gamma represent in the open-loop transfer function equation?

A

The system type number.

22
Q

First order rise time, Tr

A

2.2 tau

23
Q

First order 2% settling time, Ts

A

4 tau

24
Q

Second order 2% settling time, Ts

A

4/xiwn, where xi is the damping ratio and wn is the natural frequency.

25
Q

Second order peak time, Tp

A

π/wd

26
Q

Second order percentage overshoot, D%

A

100e^(-πxi/√(1-xi^2))

27
Q

Three effects of increasing the damping ratio

A

The settling time and overshoot decrease, which is good. The peak time increases, which is bad.

28
Q

Optimal damping ratio

A

xi = 0.7, which gives an overshoot of D% = 5%.

29
Q

Proportional controller, Kp

A

Improves rapidity, but can introduce a steady state error. This error can be reduced by increasing Kp, but this reduces stability margins.

30
Q

Proportional integral controller, Kp + Ki/s

A

The integral action can suppress the steady state error, but it also reduces the stability margins. It increases the order of the system, so it can introduce undesirable oscillations.

31
Q

Proportional derivative controller, Kp + Kds

A

Increases the stability margins, but introduces a steady state error. This can be reduced by increasing Kp and Kd, while still keeping good stability margins. The main drawback is that it introduces high frequency noise.

32
Q

Proportional integral-derivative controller

A

Kp + Ki/s + Kds