K. Ninomiya

Attitude control system design of a satellite with a magnetically suspended momentum wheel based on two-degree-of-freedom control system theory

I. Nakatani, T. Hashimoto, T. Hamasaki, 1993 .

Simulation and Validation Techniques to Establish Spacecraft Control System Performance

K. Ninomiya, D. DeBra, J. Hursh, 1984 .

A 100 ns 4Mbit (512K×8bit) CMOS EPROM

T. Watanabe, K. Ninomiya, T. Urai, 1988, ESSCIRC '88: Fourteenth European Solid-State Circuits Conference.

Development of the microprocessor-based attitude control system for ASTRO-C

T. Okamoto, F. Watanabe, Ken Maeda, 1986 .

A Novel Attitude Control Scheme for a High Energy Solar Physics Mission

T. Tanaka, K. Ninomiya, K. Maeda, 1987 .