CRC 749. — 1982. — 434 p.
This research contribution describes the analitical model upon which the software for the SAM simulation MISS is based. It includes a detailed discussion of the modelling of SAM guidance functions, the tracking process upon which they are based, and the aerodynamic responce to guidance commands.
List of Illustrations.
Coordinate system.
Guidance functions.
Proportional Navigation.
Command Guidance Model.
Homing Guidance Model.
Launch-rail orientation.
Tracking functions.
General Discussion of Tracking Servos.
Development of a Digital Servo Model.
Implementation of the Tracking Model.Flight dynamics.
Propulsion.
Performance Limits.
Aerodynamic Response.
Position and Velocity Update.Appendix A: Fortran source code listing.
Appendix B: Fortran Variable Names.
Appendix C: Cross-Reference Materials.