/*************************************************************************** TITLE: ls_gravity ---------------------------------------------------------------------------- FUNCTION: Gravity model for LaRCsim ---------------------------------------------------------------------------- MODULE STATUS: developmental ---------------------------------------------------------------------------- GENEALOGY: Created by Bruce Jackson on September 25, 1992. ---------------------------------------------------------------------------- DESIGNED BY: Bruce Jackson CODED BY: Bruce Jackson MAINTAINED BY: Bruce Jackson ---------------------------------------------------------------------------- MODIFICATION HISTORY: DATE PURPOSE BY 940111 Changed include files to "ls_types.h" and "ls_constants.h" from "ls_eom.h"; also changed DATA types to SCALAR types. EBJ $Header$ $Log$ Revision 1.1 1997/05/29 00:09:56 curt Initial Flight Gear revision. * Revision 1.2 1994/01/11 18:50:35 bjax * Corrected include files (was ls_eom.h) and DATA types changed * to SCALARs. EBJ * * Revision 1.1 1992/12/30 13:18:46 bjax * Initial revision * ---------------------------------------------------------------------------- REFERENCES: Stevens, Brian L.; and Lewis, Frank L.: "Aircraft Control and Simulation", Wiley and Sons, 1992. ISBN 0-471- ---------------------------------------------------------------------------- CALLED BY: ---------------------------------------------------------------------------- CALLS TO: ---------------------------------------------------------------------------- INPUTS: ---------------------------------------------------------------------------- OUTPUTS: --------------------------------------------------------------------------*/ #include "ls_types.h" #include "ls_constants.h" #include #define GM 1.4076431E16 #define J2 1.08263E-3 void ls_gravity( SCALAR radius, SCALAR lat, SCALAR *gravity ) { SCALAR radius_ratio, rrsq, sinsqlat; radius_ratio = radius/EQUATORIAL_RADIUS; rrsq = radius_ratio*radius_ratio; sinsqlat = sin(lat)*sin(lat); *gravity = (GM/(radius*radius)) *sqrt(2.25*rrsq*rrsq*J2*J2*(5*sinsqlat*sinsqlat -2*sinsqlat + 1) + 3*rrsq*J2*(1 - 3*sinsqlat) + 1); }