The problem of spacecraft attitude stabilization control system with limited communication
and external disturbances is investigated based on an event-triggered control scheme. In …

In an effort to pursue more advanced missions in space, improved on-board trajectory
optimization and path (re) planning capabilities are necessary. Over the past decades …

CONSTRAINED attitude motion planning for spacecraft is necessary in many mission
scenarios: for example, when the spacecraft has a sensitive instrument that may become …

This paper investigates capability and efficiency of utilizing the inverse dynamics in the
virtual domain (IDVD) method to provide the real-time updates of feasible trajectory for an …

The nanosatellite reorientation maneuver is one of the important elements of achieving the
mission goal if it is required to ensure the transfer of the nanosatellite axes from the initial to …

An experimental campaign has been conducted to evaluate the performance of two different
guidance and control algorithms on a multi-constrained docking maneuver. The evaluated …

The objective of this paper is to plan a time-optimal attitude trajectory in a relatively short
time for spacecraft with movable parts under complex pointing constraints. The constrained …

Abstract Space object observation requirements and the avoidance of specific attitudes
produce pointing constraints that increase the complexity of the attitude maneuver path …

A novel approach for minimum-time reconfiguration of satellite formations is proposed
considering the perturbation forces as control variables. Planning appropriate attitude …

The overall problem of scheduling and planning in space-borne observations has always
been a focused research to enhance the efficiency of agile optical satellites. However, few …