Digital flight control and landing system for the CH-46C helicopter Final report

Systems analysis of flight control and guidance of CH-46C helicopte

Automatic control of a liquid nitrogen cooled, closed-circuit, cryogenic pressure tunnel

The control system design, performance analysis, microprocesser based controller software development, and specifications for the Transonic Cryogenic Tunnel (TCT) are discussed. The control laws for the single-input single-output controllers were tested on the TCT simulator, and successfully demonstrated on the TCT

Automatic assembly design project 1968/9 :|breport of economic planning committee

Investigations into automatic assembly systems have been carried out. The conclusions show the major features to be considered by a company operating the machine to assemble the contact block with regard to machine output and financial aspects. The machine system has been shown to be economically viable for use under suitable conditions, but the contact block is considered to be unsuitable for automatic assembly. Data for machine specification, reliability and maintenance has been provided

Study of an attitude reference system utilizing an electrically suspended gyro final report, 1 aug. 1964 - 31 mar. 1965

Miniature electrically suspended gyroscope for spacecraft attitude reference syste

Advanced feed system component interaction analysis Quarterly status letter, 30 Jun. - 30 Sep. 1969

Dynamic model of Mars Mariner 1969 pressure regulato

Proceedings of the Space Shuttle Integrated Electronics Conference, volume 3

Proceedings of space shuttle integrated electronics conference with emphasis on data systems design - Vol.

Evaluation of star gyro torquing final report

Electrostatic gyroscope torquin

Special Libraries, October 1957

Volume 48, Issue 8https://scholarworks.sjsu.edu/sla_sl_1957/1007/thumbnail.jp