Attitude stabilization and control of earth satellites
نویسندگان
چکیده
منابع مشابه
Dynamic Modeling for Earth – Pointing Satellites to Control the Three – axis Attitude without the Attitude Information of One Axis
Various methods are presented to control the attitude of satellite due to lack of information of yaw axis attitude so far.
In this paper, a new method is used which is more general and is applicable to all types of satellites, with at least one controller. 
This method is not limited to YAW axis and can control the two other axes as well. One feature of this approach is the ability to be ...
متن کاملDynamic Modeling for Earth – Pointing Satellites to Control the Three – axis Attitude without the Attitude Information of One Axis
Various methods are presented to control the attitude of satellite due to lack of information of yaw axis attitude so far. In this paper, a new method is used which is more general and is applicable to all types of satellites, with at least one controller. This method is not limited to YAW axis and can control the two other axes as well. One feature of this approach is the ability to be modi...
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In this paper we present the design of a linear constrained MPC controller for magnetic actuated small satellites. The controller may be derived by formulating a linear constrained MPC problem as a multi-parametric quadratic program (mpQP). The solution will be a piecewise affine (PWA) function, which may be evaluated at each sample to obtain the optimal control law. We apply this approach to t...
متن کاملCoordinated Control of Satellites: the Attitude Case
In this paper an observer-controller structure for attitude synchronization of a satellite formation is presented. The design applies methods from mechanical synchronization to design a nonlinear observer and controller for satellites actuated by means of reaction wheels and magnetic torquers. In this approach one satellite is defined as the leader of the formation, while the rest are defined a...
متن کاملThe Combined Energy and Attitude Control System for Small Satellites – Earth Observation Missions
Small satellites for earth observation missions have received attention in the recent years for further optimisation. A potential approach would be to optimise the existing platforms in order to cope with their increasing mission requirements (e.g. mass, volume, etc.). In this article, the idea of combining the energy storage and attitude control systems is presented based on the flywheel techn...
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ژورنال
عنوان ژورنال: Space Science Reviews
سال: 1965
ISSN: 0038-6308,1572-9672
DOI: 10.1007/bf00177093