The two volumes of this document present an analyst manual and a users manual for a three dimensional, three degree-of-freedom trajectory simulation. The missile model described in this volume uses trimmed aerodynamic data (zero pitching moment) with the missile autopilot computations approximated in the steady state using a single time lag representation of the dynamic response. Several missile autopilot systems are approximated as are several target options. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren