Dynamics cheat sheet

More documents

Recommendations

Info

$my Latex and Tex4ht cheat sheet$

From: Performance, stability, dynamics and control of Airplanes. By Pamadi, AIAA press. Page 169 http://www.americanflyers.net/aviationlibrary/pilots_handbook/chapter_3.htm Image from http://www.americanflyers.net/aviationlibrary/pilots_handbook/chapter_3.htm 112
Image from http://www.americanflyers.net/aviationlibrary/pilots_handbook/chapter_3.htm 113
Page 1 and 2:
Dynamics cheat sheet Nasser M. Abba
Page 3 and 4:
18.7.2 Bi-Elliptic transfer orbit .
Page 5 and 6:
are the natural frequencies of the
Page 7 and 8:
Similarly, µ 2 is found ⎧ ⎫T
Page 9 and 10:
Or in full form and ⎧ ⎫ ⎡ ⎨
Page 11 and 12:
Hence The first eigen vector is Sim
Page 13 and 14:
The transformation from modal coord
Page 15 and 16:
Where F n = 2 T F 0 = 2 T ∫ T 0
Page 17 and 18:
Let z = Re { Ze iωt} , z ′ = Re
Page 19 and 20:
Now, u = Re { Ue iωt} , u ′ = Re
Page 21 and 22:
Hence at t = 0 the phase of the res
Page 23 and 24:
The following table gives the solut
Page 25 and 26:
5.3 no loading (free) mu ′′ + c
Page 27 and 28:
5.5 Impulse sin function Input is g
Page 29 and 30:
Solution to single degree of freedo
Page 31 and 32:
7 Some common formulas These defini
Page 33 and 34:
8 Derivation of the solutions of th
Page 35 and 36:
8.2.2 under-damped ζ < 1 The gener
Page 37 and 38:
When ϖ ≈ ω but less than ω, le
Page 39 and 40:
Hence the full solution is u p = p
Page 41 and 42:
8.4 Response to impulsive loading 8
Page 43 and 44:
where A = B = F 0 m 2ω √ ξ 2
Page 45 and 46:
where ∆ is very small positive qu
Page 47 and 48:
at t = t 1 ˙u (t 1 ) = −ξωe
Page 49 and 50:
8.5 references 1. Vibration analysi
Page 51 and 52:
11 Formulas sin 2 x 1cos2x 2 cos 2
Page 53 and 54:
12 Velocity and acceleration diagra
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
Page 73 and 74: 73
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
Page 89 and 90: 89
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 and 104: http://www.grc.nasa.gov/WWW/k-12/UE
Page 105 and 106: http://en.wikipedia.org/wiki/Lift_c
Page 107 and 108: http://adamone.rchomepage.com/cg_ca
Page 109 and 110: From http://www.solar-city.net/2010
Page 111: Page 184, flight dynamics principle
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.
show all

Dynamics cheat sheet

Create successful ePaper yourself

Delete template?

Save as template?