Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19650036351

Basic response relations for space vehicle attitude control using gyros.

Cannon, R. H., Jr.

View original source ↗Export metadata ↓

Abstract

Use of single-axis gyros for attitude control of space vehicles

Explore related subjects

SATELLITE ATTITUDE CONTROL GYRO-STABILIZED MOMENTUM TRANSFER ATTITUDE CONTROL

Keep this discovery

Explore connections, maps & timelines

Cannon, R. H., Jr.. 1965-01-01. Basic response relations for space vehicle attitude control using gyros.. https://ntrs.nasa.gov/citations/19650036351

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1967

Attitude instability regions of a spinning symmetric satellite in an elliptic orbit.

Attitude stability of spinning rigid symmetric satellite in elliptic orbit examined for motion about equilibrium position with spin axis normal to orbit plane

SATELLITE ATTITUDE CONTROL↗

NASA NTRS1967

Design and performance of a thermal storage resistojet.

Single nozzle thermal storage resistojet thrustor for low thrust satellite attitude and orbit control applications, noting design and performance

SATELLITE ATTITUDE CONTROL↗

NASA NTRS1967

On the application of electric propulsion to satellite orbit adjustment and station keeping.

Satellite orbit adjustment, stationkeeping and attitude control of typical earth- and sun- synchronous satellites by electric propulsion systems

SATELLITE ATTITUDE CONTROL↗