Add to ORKGThe analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabi...
Momentum management is discussed for a Large Space Structure (LSS) with the structure selected confi...
Attitude stability of an asymmetric dual-spin spacecraft incorporating a flexible joint under the in...
It is assumed that since the solar paddle attachments to the hub of the spacecraft are not rigidly l...
The air-bearing spin facility was developed to determine experimentally the effect of energy dissipa...
The stability of a dual-spin satellite system during the momentum wheel spin-up maneuver is treated ...
Stable rotating semi-rigid bodies were demonstrated analytically, and verified in flights such as Ex...
An executive summary and an analysis of the results are discussed. A user's guide for the digital co...
A dual-spin spacecraft having a momentum wheel spinning relative to a platform to provide bias momen...
Since the attitude instability experience by Explorer 1, many papers have been written on the effect...
Precession maneuver control laws for single-spin spacecraft are investigated so that nutation is con...
The applicability of dual-spin technology to a Jupiter orbiter with probe mission was investigated. ...
Nadir pointing satellites can experience large atmospheric torques during low perigee parking orbits...
The stability of spinning flexible satellites in a force-free environment was analyzed. The satellit...
The motion of the angular momentum vector in body coordinates for torque free, asymmetric dual spin ...
The analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabi...
Momentum management is discussed for a Large Space Structure (LSS) with the structure selected confi...
Attitude stability of an asymmetric dual-spin spacecraft incorporating a flexible joint under the in...
It is assumed that since the solar paddle attachments to the hub of the spacecraft are not rigidly l...
The air-bearing spin facility was developed to determine experimentally the effect of energy dissipa...
The stability of a dual-spin satellite system during the momentum wheel spin-up maneuver is treated ...
Stable rotating semi-rigid bodies were demonstrated analytically, and verified in flights such as Ex...
An executive summary and an analysis of the results are discussed. A user's guide for the digital co...
A dual-spin spacecraft having a momentum wheel spinning relative to a platform to provide bias momen...
Since the attitude instability experience by Explorer 1, many papers have been written on the effect...
Precession maneuver control laws for single-spin spacecraft are investigated so that nutation is con...
The applicability of dual-spin technology to a Jupiter orbiter with probe mission was investigated. ...
Nadir pointing satellites can experience large atmospheric torques during low perigee parking orbits...
The stability of spinning flexible satellites in a force-free environment was analyzed. The satellit...
The motion of the angular momentum vector in body coordinates for torque free, asymmetric dual spin ...
The analysis and the FORTRAN program are presented for the determination of attitude of a spin-stabi...
Momentum management is discussed for a Large Space Structure (LSS) with the structure selected confi...
Attitude stability of an asymmetric dual-spin spacecraft incorporating a flexible joint under the in...