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2V
31 32 33
yfp g fpa c F
34 35 36 37
ypow dpt P
38 39
yacc Ax Ay Az ax,k ay,k az,k
40 41 42 43 44 45
Caero CXa CYa CZa Cla Cma Cna
46 47 48 49 50 51
Cprop CXp CYp CZp Clp Cmp Cnp
52 53 54 55 56 57
FMaero Xa Ya Za La Ma Na
58 59 60 61 62 63
FMprop Xp Yp Zp Lp Mp Np
64 65 66 67 68 69
Fgrav Xgr Ygr Zgr
70 71 72
Fwind Xw Yw Zw
73 74 75
yatm r ps T μ g
76 77 78 79 80
yad1 a M qdyn
81 82 83
yad2 qc Ve Vc
84 85 86
yad3 Tt Re Rc
87 88 89
Table D.2: Logged output signals from the aircraft model. The time-trajectories of these 89
output signals are stored in the 89 corresponding columns of the matrix Out.
312 Appendix D. Data structure of the FDC model output signals
Sub- Input signals from the aircraft
vector model, logged in the matrix In
uaero de da dr df
1 2 3 4
uprop n pz
5 6
uwind uw vw ww u˙w v˙w w˙ w
7 8 9 10 11 12
Table D.3: Logged input signals for the aircraft model. The time-trajectories of these twelve
input signals are stored in the twelve corresponding columns of the matrix In.
Sub- Output signals from the system ILS example,
vector logged in the matrix yils
yils1 igs iloc
1 2
yils2 #gs Gloc
3 4
yils3 xf yf Hf dgs Rgs Rloc
5 6 7 8 9 10
yils4 LOC_flag GS_flag
11 12
Table D.4: Logged output signals from the ILS example model. The time-trajectories of these
output signals are stored in the corresponding columns of the matrix yils.
Sub- Output signals from the system VOR example,
vector logged in the matrix yvor
yVOR1 GVOR
1
yVOR2 RVOR
2
yVOR3 Cone of silence flag Range flag
3 4
yVOR4 To/From flag
5
Table D.5: Logged output signals from the VOR example model. The time-trajectories of
these output signals are stored in the corresponding columns of the matrix yvor.
Appendix F
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322 Appendix F. The Open Software License v. 2.1
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FDC 1.4 – A SIMULINK Toolbox for Flight Dynamics and Contro(111)
