UNPKG

jsbsim.js

Version:

JSBSim flight dynamics model ported to JavaScript

github.com/csbrandt/JSBSim.js

153 lines (142 loc) • 4.04 kB
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
<FDM_CONFIG NAME="{name}" VERSION="{version}"> <!-- File: {file} Author: {author} CVS Version: $Id: aircraft_template.xml,v 1.2 2003/10/18 13:21:26 ehofman Exp $ Function: {function} Notes: {notes} --> <METRICS> <!-- Data source: {source} --> AC_WINGAREA {area} <!-- square feet --> AC_WINGSPAN {span} <!-- ft --> AC_CHORD {chord} <!-- ft --> AC_HTAILAREA {area} <!-- square feet --> AC_HTAILARM {arm} <!-- ft --> AC_VTAILAREA {area} <!-- square feet --> AC_LV {arm} <!-- ft --> AC_IXX {inertia} <!-- slug-ft^2 --> AC_IYY {inertia} <!-- slug-ft^2 --> AC_IZZ {inertia} <!-- slug-ft^2 --> AC_IXZ {inertia} <!-- slug-ft^2 --> AC_EMPTYWT {weight} <!-- pounds --> AC_AERORP {X Y Z} <!-- inches --> AC_CGLOC {X Y Z} <!-- inches --> AC_EYEPTLOC {X Y Z} <!-- inches --> <!-- Pilot --> AC_POINTMASS {weight X Y Z} <!-- pounds, inches --> </METRICS> <UNDERCARRIAGE> <!-- Data source: {source} --> AC_GEAR NOSE {X Y Z} {K B D S R} {steer} {brake} {max steer} {retract} AC_GEAR LMAIN {X Y Z} {K B D S R} {steer} {brake} {max steer} {retract} AC_GEAR RMAIN {X Y Z} {K B D S R} {steer} {brake} {max steer} {retract} </UNDERCARRIAGE> <PROPULSION> <!-- Data source: {source} --> <AC_ENGINE FILE="{name}"> XLOC {X} <!-- inches --> YLOC {Y} <!-- inches --> ZLOC {Z} <!-- inches --> PITCH 0 <!-- degrees --> YAW 0 <!-- degrees --> FEED 0 FEED 1 </AC_ENGINE> <AC_THRUSTER FILE="{name}"> XLOC {X} <!-- inches --> YLOC {Y} <!-- inches --> ZLOC {Z} <!-- inches --> PITCH 0 <!-- degrees --> YAW 0 <!-- degrees --> P_FACTOR {factor} SENSE {sense} </AC_THRUSTER> <AC_TANK TYPE="FUEL" NUMBER="0"> XLOC {X} <!-- inches --> YLOC {Y} <!-- inches --> ZLOC {Z} <!-- inches --> RADIUS {radius} <!-- inches --> CAPACITY {capacity} <!-- pounds --> CONTENTS {contents} <!-- pounds --> </AC_TANK> <AC_TANK TYPE="FUEL" NUMBER="1"> XLOC {X} <!-- inches --> YLOC {Y} <!-- inches --> ZLOC {Z} <!-- inches --> RADIUS {radius} <!-- inches --> CAPACITY {capacity} <!-- pounds --> CONTENTS {contents} <!-- pounds --> </AC_TANK> </PROPULSION> <FLIGHT_CONTROL NAME="{name}"> <!-- Data source: {source} --> <COMPONENT NAME="{name}" TYPE="{type}"> </COMPONENT> </FLIGHT_CONTROL> <AERODYNAMICS> <!-- Data sources: {sources} --> <AXIS NAME="LIFT"> <COEFFICIENT NAME="{name}" TYPE="{type}"> {description} {definition} </COEFFICIENT> </AXIS> <AXIS NAME="DRAG"> <COEFFICIENT NAME="{name}" TYPE="{type}"> {description} {definition} </COEFFICIENT> </AXIS> <AXIS NAME="SIDE"> <COEFFICIENT NAME="{name}" TYPE="{type}"> {description} {definition} </COEFFICIENT> </AXIS> <AXIS NAME="ROLL"> <COEFFICIENT NAME="{name}" TYPE="{type}"> {description} {definition} </COEFFICIENT> </AXIS> <AXIS NAME="PITCH"> <COEFFICIENT NAME="{name}" TYPE="{type}"> {description} {definition} </COEFFICIENT> </AXIS> <AXIS NAME="YAW"> <COEFFICIENT NAME="{name}" TYPE="{type}"> {description} {definition} </COEFFICIENT> </AXIS> </AERODYNAMICS> <OUTPUT NAME="{name}" TYPE="{type}"> RATE_IN_HZ {rate} SIMULATION OFF ATMOSPHERE ON MASSPROPS ON AEROSURFACES ON RATES ON VELOCITIES ON FORCES ON MOMENTS ON POSITION ON COEFFICIENTS ON GROUND_REACTIONS ON FCS ON PROPULSION ON </OUTPUT> </FDM_CONFIG>