Investigation, development, and application of optimal output feedback theory
By: Neism Halyo and John R. Broussard ; prepared for Langley Research Center
Contributors: Broussard, John R; Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Information & Control Systems, Incorporated
Series: NASA contractor report -- 3828
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Control theory
Notes: "Information & Control Systems, Incorporated."

Distributed to depository libraries in microfiche

"August 1984"--Cover

Subject category 08

Includes bibliographical references

NAS1-15759
Table of contents: value: v. 1. A convergent algorithm for the stochastic infinite-time discrete optimal output feedback problem; value: v. 2. Development of an optimal, limited state feedback outer-loop digital flight control system for 3-D terminal area operation