1 /***************************************************************************
2 
3         TITLE:          basic_engine.c
4 
5 ----------------------------------------------------------------------------
6 
7         FUNCTION:       dummy engine routine
8 
9 ----------------------------------------------------------------------------
10 
11         MODULE STATUS:  incomplete
12 
13 ----------------------------------------------------------------------------
14 
15         GENEALOGY:
16 
17 
18 ----------------------------------------------------------------------------
19 
20         DESIGNED BY:    designer
21 
22         CODED BY:       programmer
23 
24         MAINTAINED BY:  maintainer
25 
26 ----------------------------------------------------------------------------
27 
28         MODIFICATION HISTORY:
29 
30         DATE    PURPOSE                                         BY
31 
32         CURRENT RCS HEADER INFO:
33 
34 $Header$
35 
36  * Revision 1.1  92/12/30  13:21:46  bjax
37  * Initial revision
38  *
39 
40 ----------------------------------------------------------------------------
41 
42         REFERENCES:
43 
44 ----------------------------------------------------------------------------
45 
46         CALLED BY:      ls_model();
47 
48 ----------------------------------------------------------------------------
49 
50         CALLS TO:       none
51 
52 ----------------------------------------------------------------------------
53 
54         INPUTS:
55 
56 ----------------------------------------------------------------------------
57 
58         OUTPUTS:
59 
60 --------------------------------------------------------------------------*/
61 #include <math.h>
62 #include "ls_types.h"
63 #include "ls_constants.h"
64 #include "ls_generic.h"
65 #include "ls_sim_control.h"
66 #include "ls_cockpit.h"
67 #include "basic_aero.h"
68 
69 extern SIM_CONTROL      sim_control_;
70 
basic_engine(SCALAR dt,int init)71 void basic_engine( SCALAR dt, int init ) {
72 
73   // c172
74   //    F_X_engine = Throttle_pct * 421;
75   // neo 2m slope
76   F_X_engine = Throttle_pct * 8;
77   F_Y_engine = 0.0;
78   F_Z_engine = 0.0;
79   M_l_engine = 0.0;
80   M_m_engine = 0.0;
81   M_n_engine = 0.0;
82 
83 
84   //  printf("Throttle_pct %f\n", Throttle_pct);
85   //  printf("F_X_engine %f\n", F_X_engine);
86 
87 
88 }
89 
90 
91