Attitude Motion of Asymmetric Dual-Spin Spacecraft

DOI10.2514/3.56136zbMath0541.70038OpenAlexW2064647424MaRDI QIDQ3327802

Ping-Huei Shu, John E. Cochran, Stephen D. Rew

Publication date: 1982

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.56136

zbMATH Keywords

analytical solutionEulerian angleselliptic integralsJacobian elliptic functionsdual-spin spacecraftangle of relative rotationattitude motion of an asymmetric gyrostatone degree of freedom in relative rotationResonance curvessystem of two rigid bodies

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Astronomy and astrophysics (85A99) Orbital mechanics (70M20)

Related Items (16)

Behavior of a free dual-spin gyrostat with different ratios of inertia moments ⋮ Dynamics and control of dual-spin gyrostat spacecraft with changing structure ⋮ On the dynamics of a gyrostat on Lagrangian equilibria in the three body problem ⋮ Dynamics and chaos control of gyrostat satellite ⋮ Stationary solutions of a small gyrostat in the Newtonian field of two bodies with equal masses ⋮ On the stability of the permanent rotations of a charged rigid body-gyrostat ⋮ Stability analysis of resonant rotation of a gyrostat in an elliptic orbit under third-and fourth-order resonances ⋮ On sufficient conditions of stability of the permanent rotations of a heavy triaxial gyrostat ⋮ Integrable cases in the dynamics of axial gyrostats and adiabatic invariants ⋮ Phase flow of an axially symmetrical gyrostat with one constant rotor ⋮ Exact solution of a triaxial gyrostat with one rotor ⋮ Stability of the permanent rotations of an asymmetric gyrostat in a uniform Newtonian field ⋮ A complex analytic solution for the attitude motion of a near-symmetric rigid body under body-fixed torques ⋮ Spin Rotor Stabilization of a Dual-Spin Spacecraft with Time Dependent Moments of Inertia ⋮ CHAOS IN THE REORIENTATION PROCESS OF A DUAL-SPIN SPACECRAFT WITH TIME-DEPENDENT MOMENTS OF INERTIA ⋮ Prediction of swerving motion of a dual-spin projectile with lateral pulse jets in atmospheric flight.

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