Abstract: The angular motion synthesis algorithm for the trajectory on the Earth’s surface tracking for remote sensing satellite is developed. Two types of sensors are considered, i.e. CCD-line and CCD-matrix. Various types of scanning trajectory parameterization including the Hermit spline are discussed. The control method which stabilizes the motion synthesized is developed.Note: Research direction:Theoretical and applied problems of mechanic
Abstract: Some problems on robust gyromoment motion control of agile spacecraft (SC) for remote sens...
Abstract: The paper presents the technique for determining attitude motion of a satellite ...
Since the dawn of the Space Age, over six thousand satellites have been launched into Earth orbit. T...
The article considers a spacecraft for remote sensing of the Earth with high-resolution or ultra-hig...
Abstract: The angular motion synthesis algorithm for remote sensing satellite is developed...
Abstract: Problem of angular motion synthesis for interplanetary flight is considered. Con...
The article deals with problems associated with determining permissible accuracy of Earth remote sen...
International audienceSatellites for observation missions, or imagery satellites, have increased dra...
Abstract: Problems on guidance, onboard signal processing and robust gyromoment motion control of ag...
This paper focuses on the trajectory planning that optical satellites approach the geostationary (GE...
Abstract: The problems and the design philosophy of precision autonomous gyroscopic attitude referen...
We present simple methods for attitude guidance and control of the land-survey mini-satellites, algo...
The spacecraft controllability of the angular motion is possible only with operability of the attitu...
Abstract: The method of attitude parameters determination of the passive gravity-gradient ...
Abstract: We consider the reconstruction of spacecraft attitude motion by measurements of ...
Abstract: Some problems on robust gyromoment motion control of agile spacecraft (SC) for remote sens...
Abstract: The paper presents the technique for determining attitude motion of a satellite ...
Since the dawn of the Space Age, over six thousand satellites have been launched into Earth orbit. T...
The article considers a spacecraft for remote sensing of the Earth with high-resolution or ultra-hig...
Abstract: The angular motion synthesis algorithm for remote sensing satellite is developed...
Abstract: Problem of angular motion synthesis for interplanetary flight is considered. Con...
The article deals with problems associated with determining permissible accuracy of Earth remote sen...
International audienceSatellites for observation missions, or imagery satellites, have increased dra...
Abstract: Problems on guidance, onboard signal processing and robust gyromoment motion control of ag...
This paper focuses on the trajectory planning that optical satellites approach the geostationary (GE...
Abstract: The problems and the design philosophy of precision autonomous gyroscopic attitude referen...
We present simple methods for attitude guidance and control of the land-survey mini-satellites, algo...
The spacecraft controllability of the angular motion is possible only with operability of the attitu...
Abstract: The method of attitude parameters determination of the passive gravity-gradient ...
Abstract: We consider the reconstruction of spacecraft attitude motion by measurements of ...
Abstract: Some problems on robust gyromoment motion control of agile spacecraft (SC) for remote sens...
Abstract: The paper presents the technique for determining attitude motion of a satellite ...
Since the dawn of the Space Age, over six thousand satellites have been launched into Earth orbit. T...