Attitude dynamics and control of satellites orbiting rotating asteroids

DOI10.1007/S00707-007-0508-YzbMath1151.70331OpenAlexW2122657068MaRDI QIDQ943061

B. E. Eshmatov

Publication date: 8 September 2008

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00707-007-0508-y

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (5)

Neural network control for the probe landing based on proportional integral observer ⋮ Attitude analysis and robust adaptive backstepping sliding mode control of spacecrafts orbiting irregular asteroids ⋮ Periodic attitudes and bifurcations of a rigid spacecraft in the second degree and order gravity field of a uniformly rotating asteroid ⋮ Orbital dynamics and equilibrium points around an asteroid with gravitational orbit-attitude coupling perturbation ⋮ On the nonlinear stability of relative equilibria of the full spacecraft dynamics around an asteroid

Uses Software

• Unnamed Item

Cites Work

• Contribution of earth oblateness to gravity torque on a satellite.

This page was built for publication: Attitude dynamics and control of satellites orbiting rotating asteroids