This paper focuses on the design of a new optical cone and pendulum scanning imaging
mode for micro-nanosatellites. This kind of satellite uses a high-resolution camera with a …

The ground-based spacecraft dynamics simulator plays an important role in the
implementation and validation of attitude control scenarios before a mission. The …

The present paper summarizes the testing work carried out in relation to the UPMSat-2
Attitude, Control and Determination Subsystem (ADCS) sensors. The ACDS of this satellite …

This paper introduces a novel active nutation/wobble rejection control method for spinning
satellites enduring thrusting disturbances and reaction wheel limitations. Our approach …

Most of the low-cost NanoSats, which run on the low-earth orbits and have no severe
pointing requirement, usually adopt magnetic-based attitude control scheme as an important …

An attitude control strategy for an under-actuated spacecraft with two reaction wheels is
proposed, using the active assistance of solar radiation pressure torque. By changing the …

Accepted: 20 July 2019 In many space applications, the spacecraft (SC) must have good
agility performance, which depends heavily on the capability of attitude control system. This …

This paper focuses on a single-axis control of a wheeled spin satellite while the entire
angular momentum is not zero. The presented technique includes a feedback control law …

The present research work consists of the description of the work carried out within the
framework of the UPMSat-2 project related to its attitude determination and control …

抄録 This paper is concerned with the control of the dual-spin turn (DST) of a spacecraft to
regulate the spacecraft attitude. The DST is a method for attitude stabilization of a rotating …