Computer considerations for real time simulation of a generalized rotor model, Volume 2877
R. M. Howe, L. E. Fogarty, United States. National Aeronautics and Space Administration, University of Michigan
National Aeronautics and Space Administration, 1977 - Games - 108 pages
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CONVENTIONAL HYBRID SIMULATION
3 other sections not shown
acceleration less gravity aerodynamic forces aircraft c.g. analog circuit angle of attack angular acceleration angular velocity components axis components axis system blade equations blade segment blade-span axes block bmax body axes body-axis c s max computing blade cosB damping ratio digital computer Dimensionless components equations of motion Euler angles Figure force components formula frequency ft ft given in Eq hinge point hub axes hub-axis hybrid mechanization hybrid simulation I-frame inertia inertial reference frame integration steps jth blade kth segment max max max max p max normalizing factor PJ PJ PJ pyj yj pzj zj real-time real-time computer respect rj pj rj rj rj rj s max rotating shaft axes rotor rotor blades rotor system s s s S-frame Scaling constant Section smax span axes variables yawed angle