Add to ORKGAbstract: Typical magneto-gyroscopic attitude control system failures are considered, “Chibis-M” microsatellite is used as an example. Mission recovery for each case is investigated. It is impossible to upload new attitude control algorithms on board. Gravitational boom is an auxiliary component of the attitude control system element and it is considered separately.Note: Research direction:Theoretical and applied problems of mechanic
Actuator failures onboard spacecraft often lead to unsatisfied control performances or even the lose...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Ca...
An actuator fault-tolerant attitude control was reported. Two kinds of spacecraft actuator failures ...
this paper we review the main results in the area of active control of spacecraft with one actuator ...
Spacecraft play an increasingly important role in various areas of modern society, such as telecommu...
Thousands of satellites are now in operation for various purposes such as communication, navigation,...
The spacecraft controllability of the angular motion is possible only with operability of the attitu...
Spacecraft perform a variety of useful tasks in our day-to-day life. These are such that spacecraft ...
Abstract The stability and singularity problem of agile small satellite (ASS) with actuator failure ...
This paper deals with the Attitude Determination And Control Subsystem (ADACS) of the SMART microsat...
Impulsive or time-decaying disturbances of sufficient magnitude will cause a gravitygradient control...
In the last decades, access to space has become more affordable thanks to the introduction of CubeSa...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
This thesis presents a method for fault diagnosis in spacecraft attitude control system. The focus o...
SMART (Scientific Microsatellite for Advanced Research and Technology) is a project of the two Unive...
Actuator failures onboard spacecraft often lead to unsatisfied control performances or even the lose...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Ca...
An actuator fault-tolerant attitude control was reported. Two kinds of spacecraft actuator failures ...
this paper we review the main results in the area of active control of spacecraft with one actuator ...
Spacecraft play an increasingly important role in various areas of modern society, such as telecommu...
Thousands of satellites are now in operation for various purposes such as communication, navigation,...
The spacecraft controllability of the angular motion is possible only with operability of the attitu...
Spacecraft perform a variety of useful tasks in our day-to-day life. These are such that spacecraft ...
Abstract The stability and singularity problem of agile small satellite (ASS) with actuator failure ...
This paper deals with the Attitude Determination And Control Subsystem (ADACS) of the SMART microsat...
Impulsive or time-decaying disturbances of sufficient magnitude will cause a gravitygradient control...
In the last decades, access to space has become more affordable thanks to the introduction of CubeSa...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
This thesis presents a method for fault diagnosis in spacecraft attitude control system. The focus o...
SMART (Scientific Microsatellite for Advanced Research and Technology) is a project of the two Unive...
Actuator failures onboard spacecraft often lead to unsatisfied control performances or even the lose...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.Ca...
An actuator fault-tolerant attitude control was reported. Two kinds of spacecraft actuator failures ...