MODERN APPROACHES TO OPTIMIZING THE PAYLOAD AND ENERGY CONSUMPTION OF THE ONBOARD COMPLEX FOR CONTROLLING SMALL SPACECRAFT IN LOW EARTH ORBITS
Abstract. Small spacecraft, especially CubeSat-type nanosatellites, often face the problem of maintaining an energy balance due to their limited size and low power sources. The main advantages of such spacecraft are their relatively low cost, rapid development, and suitability for conducting scientific research and technological experiments. However, their small size and mass impose strict limitations […]