$Header$
$Log$
+Revision 1.1 2002/09/10 01:14:01 curt
+Initial revision
+
+Revision 1.20 2001/07/30 20:53:54 curt
+Various MSVC tweaks and warning fixes.
+
Revision 1.19 2001/03/02 21:37:01 curt
Added a first pass at a C++ sound manager class.
{
char rcsid[] = "$Id$";
#define NUM_WHEELS 4
-char gear_strings[NUM_WHEELS][12]={"nose","right main", "left main", "tail skid"};
+// char gear_strings[NUM_WHEELS][12]={"nose","right main", "left main", "tail skid"};
/*
* Aircraft specific initializations and data goes here
*/
{ -1.47, -3.58, 6.71 }, /*left main*/
{ -15.67, 0, 2.42 } /*tail skid */
};
- static DATA gear_travel[NUM_WHEELS] = /*in Z-axis*/
- { -0.5, 2.5, 2.5, 0};
+ // static DATA gear_travel[NUM_WHEELS] = /*in Z-axis*/
+ // { -0.5, 2.5, 2.5, 0};
static DATA spring_constant[NUM_WHEELS] = /* springiness, lbs/ft */
{ 1200., 900., 900., 10000. };
static DATA spring_damping[NUM_WHEELS] = /* damping, lbs/ft/sec */
DATA d_wheel_cg_local_v[3]; /* wheel offset from cg, N-E-D */
DATA d_wheel_rwy_local_v[3]; /* wheel offset from rwy, N-E-U */
DATA v_wheel_cg_local_v[3]; /*wheel velocity rel to cg N-E-D*/
- DATA v_wheel_body_v[3]; /* wheel velocity, X-Y-Z */
+ // DATA v_wheel_body_v[3]; /* wheel velocity, X-Y-Z */
DATA v_wheel_local_v[3]; /* wheel velocity, N-E-D */
DATA f_wheel_local_v[3]; /* wheel reaction force, N-E-D */
- DATA altitude_local_v[3]; /*altitude vector in local (N-E-D) i.e. (0,0,h)*/
- DATA altitude_body_v[3]; /*altitude vector in body (X,Y,Z)*/
- DATA temp3a[3], temp3b[3], tempF[3], tempM[3];
+ // DATA altitude_local_v[3]; /*altitude vector in local (N-E-D) i.e. (0,0,h)*/
+ // DATA altitude_body_v[3]; /*altitude vector in body (X,Y,Z)*/
+ DATA temp3a[3];
+ // DATA temp3b[3];
+ DATA tempF[3];
+ DATA tempM[3];
DATA reaction_normal_force; /* wheel normal (to rwy) force */
DATA cos_wheel_hdg_angle, sin_wheel_hdg_angle; /* temp storage */
DATA v_wheel_forward, v_wheel_sideward, abs_v_wheel_sideward;