International audienceWe have considered some principal problems on attitude determination and control of the land-survey satellites placed on the orbit altitudes from 600 up to 1000 km. We present elaborated methods for in-flight verification and tuning of the attitude control system with animation of a satellite motion
— The paper outlines orbit and attitude control problems of a long-distance (>100 km) two-satellite ...
The paper describes the development of a microsatellite attitude determination and control subsystem...
Présentation PosterInternational audienceHigh fidelity satellite simulators are required for the val...
International audienceWe have considered some principal problems on attitude determination and contr...
We present simple methods for attitude guidance and control of the land-survey mini-satellites, algo...
International audienceContemporary information mini-satellites have general mass up to 500 kg and ar...
The paper outlines orbit and attitude control problems of a long-distance (>100 km) two-satellite fo...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
The mass and cost requirements of high-accuracy satellite pointing systems often inhibit the potenti...
Scientific exploration of near-earth space and high altitudes within earth's atmosphere greatly enha...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
A semi-physical simulation platform for attitude determination and control system is proposed to ver...
The attitude determination and control system (ADCS) for spacecraft is responsible for determining i...
The DLR Institute of Space Systems located in Bremen commissioned a new laboratory for experiments ...
M. Tech. Electrical EngineeringDeals with nonlinear methods for magnetic attitude control and reacti...
— The paper outlines orbit and attitude control problems of a long-distance (>100 km) two-satellite ...
The paper describes the development of a microsatellite attitude determination and control subsystem...
Présentation PosterInternational audienceHigh fidelity satellite simulators are required for the val...
International audienceWe have considered some principal problems on attitude determination and contr...
We present simple methods for attitude guidance and control of the land-survey mini-satellites, algo...
International audienceContemporary information mini-satellites have general mass up to 500 kg and ar...
The paper outlines orbit and attitude control problems of a long-distance (>100 km) two-satellite fo...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
The mass and cost requirements of high-accuracy satellite pointing systems often inhibit the potenti...
Scientific exploration of near-earth space and high altitudes within earth's atmosphere greatly enha...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
A semi-physical simulation platform for attitude determination and control system is proposed to ver...
The attitude determination and control system (ADCS) for spacecraft is responsible for determining i...
The DLR Institute of Space Systems located in Bremen commissioned a new laboratory for experiments ...
M. Tech. Electrical EngineeringDeals with nonlinear methods for magnetic attitude control and reacti...
— The paper outlines orbit and attitude control problems of a long-distance (>100 km) two-satellite ...
The paper describes the development of a microsatellite attitude determination and control subsystem...
Présentation PosterInternational audienceHigh fidelity satellite simulators are required for the val...