Searched refs:engineOmega (Results 1 – 4 of 4) sorted by relevance
403 M_n_aero += polarInertia * engineOmega * Q_body; in uiuc_force_moment()405 M_m_aero += -polarInertia * engineOmega * R_body; in uiuc_force_moment()
164 engineOmega = minOmega + Throttle[3] * (maxOmega - minOmega); in uiuc_engine()
2237 fout << polarInertia * engineOmega * Q_body << " "; in uiuc_recorder()2242 fout << -polarInertia * engineOmega * R_body << " "; in uiuc_recorder()2252 fout << (engineOmega * 60 / (2 * LS_PI)) << " "; in uiuc_recorder()
1049 double minOmega, maxOmega, minOmegaRPM, maxOmegaRPM, engineOmega, polarInertia; member1056 #define engineOmega aircraft_->engineOmega macro