Modeling and effect analysis of space nutation target detumbling using rotatable flexible rod
An optimal nutation reduction method for contact de-tumbling of satellites
Linear Stability Boundary of a Spinning Spacecraft with a Ball-in-Tube Damper
Optimal contact control for space debris detumbling and nutation damping
Forced nutations of a two-layer Earth in canonical formulation with dissipative Hori-like kernel
Ajisai spin-axis precession and rotation-period variations from photometric observations
Ajisai spin-axis precession and rotation-period variations from photometric observations
Active nutation control of an asymmetric spacecraft using an axial reaction wheel
Magnetospheric Multiscale Mission Attitude Dynamics: Observations from Flight Data
Influence of ITRS/GCRS implementation for astrodynamics: Coordinate transformations
Convex Solution to a Joint Attitude and Spin-Rate Estimation Problem
In-flight quality evaluation of attitude measurements from STECE APS-01 star tracker
Stability of Spinning Satellite Under Axial Thrust, Internal Mass Motion, and Damping
Chaos and its avoidance in spinup dynamics of an axial dual-spin spacecraft
Motion of a descent capsule relative to its center of mass when deploying the orbital tether system
Motion of a descent capsule relative to its center of mass when deploying the orbital tether system
VLBI: Radio Interferometry for Celestial and Terrestrial Frames
Time Frequency Analysis of Spacecraft Propellant Tank Spinning Slosh
Free librations of the two-layer Moon and the possibilities of their detection
Inner core wobble and free core nutation of pulsar PSR B1828-11
Mantle Heterogeneity and Tidal Deformation
Optimal Attitude Maneuver Execution for the Advanced Composition Explorer (ACE) Mission
Telemetry down-Link Doppler as an Attitude Sensor for Spin Stabilized Spacecraft
A spinning filled fluid reservoir for momentum biased spacecraft nutation damping
Effectiveness of Large Booms as Nutation Dampers for Spin Stabilized Spacecraft
Attitude and payload control system for INTELSAT VI
Dual-spin-spacecraft nutation control using articulated payloads
Accurate Spacecraft Attitude Estimation with the Esa Starmapper
Study of Spacecraft Attitude Reconstitution Using the ESA Starmapper
MAGE Orbital Propulsion Unit (MOPU) Definition Study. Volume 1: Technical