This paper investigates the attitude tracking control of multi-body spacecraft with external disturbance torques and parameters perturbations.

This paper investigates the robust control of large angle maneuver for the multi-body spacecraft with model uncertainties.

Lagrange s equations in quasi-coordinates are used for dynamics modeling of a multi-body spacecraft consisting of a rigid center body, several flexible appendages and an antenna.

Flexible Multibody Spacecraft Dynamic Modeling and Attitude Control;

The research of interoperability between Multi-spacecraft has become a hot issue in the field of aerospace,the establishment of a high confidence level of the simulation system has become the issue in depth to engineering applications.

Nonholonomic motion planning for the attitude of rigid spacecraft with two momentum wheel actuators;

In terms of this characteristic, the three-dimensional attitude control problem of the rigid spacecraft with three manipulators is discussed in the paper.

For rigid spacecraft attitude tracking system with uncertain inertia matrix and external disturbances,an adaptive sliding mode approach is presented.

The applications of GPS in a multi spacecraft system with kinematical restraint but no structural restraint and force action to each other are studied in this paper.

The problem of optimized reentry-trajectory design for lift-body was studied.