DEVICE FOR CONSTRUCTING THE LOCAL VERTICAL FOR NANOSPACECRAFT
Annotation
A device and a method for constructing local vertical for nanospacecraft based on the sight of the horizon of the Earth in the visible wavelength range are proposed. The use of such a system on the nanosatellite is reported to allow determination of the local vertical direction with accuracy comparable with the accuracy of infrared local vertical detectors, and also to provide significant gains in mass and power consumption. The disadvantages of the system include the inability to determine the orientation on the shady part of the orbit, as well as flashing of the image when struck by sunlight in the frame. Presented results of numerical experiments demonstrate that the proposed system works in a wide range of orientation angles. A semi-natural experiment to determine the pitch angle by processing video images received from camera is carried out. Results of the experiment confirm that the accuracy of the developed system for constructing local vertical of spacecraft based on video processing is comparable to the precision provided by infrared detectors of local vertical.
Keywords
Постоянный URL
Articles in current issue
- PERSPECTIVES OF SMALL SIZE SPACECRAFT DEVELOPMENT FOR VARIOUS PURPOSES AT JSC RUSSIAN SPACE SYSTEMS
- CONSTRUCTION OF SMALL SPACECRAFT CLUSTERS
- INVESTIGATION OF SOLAR-TERRESTRIAL CONNECTION AND NEAR-EARTH PLASMA WITH THE USE OF SMALL SPACECRAFTS
- THE SPECIFICS OF SPACE RESEARCH ON MICRO-SATELLITE PLATFORMS INTEGRATED INTO THE INFRASTRUCTURE OF RUSSIAN SEGMENT OF THE ISS
- CHOICE OF THE DESIGN PARAMETERS OF AERODYNAMICALLY STABILIZED NANOSATELLITE
- ELECTRICAL POWER SUBSYSTEM DESIGN FOR SAMSAT NANOSATELLITE
- STUDY OF INHOMOGENEOUS STRUCTURE OF THE IONOSPHERE USING SIMULTANEOUS MEASUREMENTS BY NANOSATELLITES OF CUBESAT STANDARD
- ANALYSIS OF POSSIBLE FAILURES OF STANDARD NANOSATELLITE
- PROSPECTS OF REALIZATION OF PROTO-FLIGHT APPROACH IN NANOSATELLITE GROUND TESTING
- SMALL SPACECRAFT LAUNCHING SYSTEM
- COMPACT AUTOMATIC SYSTEM FOR MANAGED LAUNCH OF NANOSATELLITES
- PROJECT OF NANOSATELLITE GROUP SEPARATION AT CLUSTER LAUNCHING FROM AN ORBITAL STAGE
- SPECIAL FEATURES OF LOW-ALTITUDE AERODYNAMICALLY STABILIZED NANOSATELLITE MOVEMENT