๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

On-orbit control system performance of the ROSAT spacecraft

โœ Scribed by M. Bollner

Publisher
Elsevier Science
Year
1991
Tongue
English
Weight
592 KB
Volume
25
Category
Article
ISSN
0094-5765

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

Long-term performance of the passive the
Long-term performance of the passive thermal control systems of the IRAS spacecraft
โœ P.V. Mason ๐Ÿ“‚ Article ๐Ÿ“… 1988 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 407 KB

Degradat=on of passwe thermal control systems m space =s a matter of senous concern and has been observed =n many missions We report here the performance of the pass=ve thermal control systems of the Infrared Astronomical Satelhte (IRAS) over a period of three years An extenor temperature of 200 K a

THE INFLUENCE OF CONTROL SYSTEM DESIGN O
THE INFLUENCE OF CONTROL SYSTEM DESIGN ON THE PERFORMANCE OF VIBRATORY GYROSCOPES
โœ P.W. LOVEDAY; C.A. ROGERS ๐Ÿ“‚ Article ๐Ÿ“… 2002 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 237 KB

Understanding the in#uence of the control system on the performance of vibratory gyroscopes is important during the design of such devices. The ability of the control system to reduce the e!ects of resonator imperfections, on the gyroscope performance, was investigated. The analysis of the control p

Attitude stabilization of a rigid spacec
Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
โœ Hariharan Krishnan; Mahmut Reyhanoglu; Harris McClamroch ๐Ÿ“‚ Article ๐Ÿ“… 1994 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 501 KB

The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet actuators about only two of its principal axes is considered. If the uncontrolled principal axis of the spacecraft is not an axis of symmetry, then the complete spacecraft dynamics are small time local