72926 ⎘
Cosmonautic vehicles; Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles; Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
Positioning computer for a satellite having an optical inter-satellite communication system on an anti-Earth face
#2Autonomous Satellite Navigation
#3METHODS AND SYSTEMS FOR ORBIT ESTIMATION OF A SATELLITE
#4Systems and Methods for Adjusting the Orbit of a Payload
#5SYSTEM AND METHOD FOR DETERMINING AN INITIAL ORBIT OF SATELLITES POST DEPLOYMENT
#6Methods and apparatus for performing propulsion operations using electric propulsion systems
#7Model predictive control of spacecraft
#8Model predictive control of spacecraft
#9Methods and apparatus for performing propulsion operations using electric propulsion systems
#10Torque generation system, attitude control system for spacecraft, and relative position and velocity control system for spacecraft
#11Menu-type design method for GEO satellite control system based on optimized information integration
#12Attitude determination using earth horizon sensors
#13Apparatus and method for controlling a satellite
#14Methods and apparatus for performing propulsion operations using electric propulsion systems
#15Apparatus and method for controlling a satellite
#16TORQUE GENERATION SYSTEM, ATTITUDE CONTROL SYSTEM FOR SPACECRAFT, AND RELATIVE POSITION AND VELOCITY CONTROL SYSTEM FOR SPACECRAFT
#17Solar energy conversion and transmission system and method
#18Methods and apparatus for performing propulsion operations using electric propulsion systems
#19Attitude determination using infrared earth horizon sensors
#20Propulsion system for controlling the orbit and controlling the attitude of a satellite
#21Systems and methods for a self-deploying vehicle drag device
#22Spacecraft momentum management using solar array
#23Method and computer program product for controlling inertial attitude of an artificial satellite by applying gyroscopic precession to maintain the spin axis perpendicular to sun lines
#24Algorithm for simultaneous attitude maneuver and momentum dumping
#25Method for determining the position of a spacecraft with the aid of a direction vector and an overall spin measurement
#26Method, satellite, and a system or an arrangement with at least one satellite for detecting natural or artificial objects, and the use thereof in the execution of said method
#27Systems and method of controlling a spacecraft using attitude sensors
#28System for determing and controlling inertial attitude, for navigation, and for pointing and/or tracking for an artificial satellite employing and optical sensor and a counter-rotational optical mirror, and terrestrial-based testing system for assessing inertial attitude functions of an artificial satellite
#29Method and apparatus for determining a satellite attitude using crosslink reference signals
#30METHOD AND APPARATUS TO DETERMINE A PLANET VECTOR
#31Method and receiver for the simultaneous detection and evaluation of at least two electro-magnetic signals
#32High temperature oxidation resistant material for spacecraft, hot structure part, spacecraft, and method for producing high temperature oxidation resistant material for spacecraft
#33Solar control method for spacecraft
#34System and method to enhance attitude estimation for transfer orbit maneuver
#35Process for determining the position of a spacecraft with the aid of a directional vector and a total angular momentum measurement
#36Predicting, bounding and mitigating satellite attitude disturbances arising from infrared earth sensors for satellites in inclined, elliptical orbits