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Dynamics cheat sheet Nasser M. Abba
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18.7.2 Bi-Elliptic transfer orbit .
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are the natural frequencies of the
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Similarly, µ 2 is found ⎧ ⎫T
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Or in full form and ⎧ ⎫ ⎡ ⎨
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Hence The first eigen vector is Sim
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The transformation from modal coord
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Where F n = 2 T F 0 = 2 T ∫ T 0
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Let z = Re { Ze iωt} , z ′ = Re
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Now, u = Re { Ue iωt} , u ′ = Re
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Hence at t = 0 the phase of the res
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The following table gives the solut
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5.3 no loading (free) mu ′′ + c
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5.5 Impulse sin function Input is g
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Solution to single degree of freedo
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7 Some common formulas These defini
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8 Derivation of the solutions of th
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8.2.2 under-damped ζ < 1 The gener
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When ϖ ≈ ω but less than ω, le
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Hence the full solution is u p = p
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8.4 Response to impulsive loading 8
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where A = B = F 0 m 2ω √ ξ 2
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where ∆ is very small positive qu
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at t = t 1 ˙u (t 1 ) = −ξωe
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8.5 references 1. Vibration analysi
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11 Formulas sin 2 x 1cos2x 2 cos 2
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- Page 55 and 56: 12.3 spring pendulum with block mov
- Page 57 and 58: 13 Velocity and acceleration of rig
- Page 59 and 60: 14.2 3D Not Using vehicle dynamics
- Page 61 and 62: 14.2.2 Derivation for τ = Iω in 3
- Page 63 and 64: 15 Wheel spinning precession x Mg
- Page 65 and 66: 18 Astrodynamics 18.1 Ellipse main
- Page 67 and 68: magnitude of ⃗r period T mean sat
- Page 69 and 70: 18.3 Flight path angle for ellipse
- Page 71 and 72: This diagram below from Orbital mec
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- Page 75 and 76: 18.7.3 semi-tangential elliptical t
- Page 77 and 78: 18.8.1 Rocket equation with plane c
- Page 79 and 80: 18.10 interplanetary transfer orbit
- Page 81 and 82: 2. Find speed of second planet V 2
- Page 83 and 84: 1 mu = 324859; 2 alt = 1475.776; 3
- Page 85 and 86: 18.11.3 Two satellite, separate orb
- Page 87 and 88: 1 TOF:=hohmann_rendezvous_2(theta=0
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- Page 91 and 92: 18.14 Orbit changing by low contiuo
- Page 93 and 94: C r below is the core chord of the
- Page 95 and 96: 1 C L = ∂C L ∂α α = C Lα α
- Page 97 and 98: 1 2 3 C Lwb = ∂C L wb ∂α wb α
- Page 99 and 100: 2. stall from http://en.wikipedia.o
- Page 101 and 102: http://en.wikipedia.org/wiki/Flight
- Page 103: http://www.grc.nasa.gov/WWW/k-12/UE
- Page 107 and 108: http://adamone.rchomepage.com/cg_ca
- Page 109 and 110: From http://www.solar-city.net/2010
- Page 111 and 112: Page 184, flight dynamics principle
- Page 113 and 114: Image from http://www.americanflyer
- Page 115 and 116: From FAA pilot’s handbook I do no
- Page 117 and 118: zero-lift angle The angle of attack
- Page 119: Image from http://www.aerospaceweb.