Tomeki

Explore Books on
attitude stability

1-8 of 8 Books

View Three-axis stabilization of spacecraft using parameter-independent nonlinear quaternion feedback By S. M. Joshi

Three-axis stabilization of spacecraft using parameter-independent nonlinear quaternion feedback

Three-axis stabilization of spacecraft using parameter-independent nonlinear quaternion feedback

By S. M. Joshi

View Attitude stability and performance of a dual-spin satellite with large flexible appendages By D. B. Cherchas

Attitude stability and performance of a dual-spin satellite with large flexible appendages

Attitude stability and performance of a dual-spin satellite with large flexible appendages

By D. B. Cherchas

View Flexible robotic manipulator in space By P. Th. L. M. van Woerkom

Flexible robotic manipulator in space

Flexible robotic manipulator in space

By P. Th. L. M. van Woerkom

View Attitude stability of articulated gravity-oriented satellites By Bernard Etkin

Attitude stability of articulated gravity-oriented satellites

Attitude stability of articulated gravity-oriented satellites

By Bernard Etkin

View Stability diagrams for a rigid gyrostat in a circular orbit By P. C. Hughes

Stability diagrams for a rigid gyrostat in a circular orbit

Stability diagrams for a rigid gyrostat in a circular orbit

By P. C. Hughes

View Attitude stability of articulated gravity-oriented satellites By H. Maeda

Attitude stability of articulated gravity-oriented satellites

Attitude stability of articulated gravity-oriented satellites

By H. Maeda

View Finite-element analysis of CTS-like flexible spacecraft By Phung Khac Nguyen

Finite-element analysis of CTS-like flexible spacecraft

Finite-element analysis of CTS-like flexible spacecraft

By Phung Khac Nguyen

View The attitude stability of a flexible rod satellite placed at an equilateral Lagrangian point in the restricted three-body problem By Gary Waters

The attitude stability of a flexible rod satellite placed at an equilateral Lagrangian point in the restricted three-body problem

The attitude stability of a flexible rod satellite placed at an equilateral Lagrangian point in the restricted three-body problem

By Gary Waters