Accession Number:

AD0729854

Title:

Digital Missile Controller Design and Analysis Information.

Descriptive Note:

Final technical rept.,

Corporate Author:

FLORIDA UNIV GAINESVILLE COLL OF ENGINEERING

Report Date:

1971-05-01

Pagination or Media Count:

300.0

Abstract:

The report documents design and analysis information developed for the practical design and analysis of digital controllers of U.S. Army servo-actuator-vane controlled missiles. This information is in the form of a development of the design and analysis methods for high-order, multi-loop, multi-rate digitally controlled system, and computer programs for the practical analysis and design of such systems. The methods developed herein are multi-loop, multi-rate simulation for time, and frequency responses of the digital guidance and control system with computing delays classical frequency domain design and analysis of the multi-loop, multi-rate, open and closed-loop systems via the modified z-transform emulation of the flight control computer on an IBM computer for memory, computing time and error analysis automated modern design of the digital compensators by solution of the linear-quadratic-loss optimization problem and the Kalman filter and, the determination of the optimization problem from the solution of the inverse problem which transforms classical specifications into modern specifications. Author

Subject Categories:

  • Computer Programming and Software
  • Computer Hardware
  • Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE