Orbit Determination and Differential-drag Control of Planet Labs Cubesat Constellations
read the original abstract
We present methodology and mission results from orbit determination of Planet Labs nanosatellites and differential-drag control of their relative motion. Orbit determination (OD) is required on Planet Labs satellites to accurately predict the positioning of satellites during downlink passes and we present a scalable OD solution for large fleets of small satellites utilizing two-way ranging. In the second part of this paper, we present mission results from relative motion differential-drag control of a constellation of satellites deployed in the same orbit.
This paper has not been read by Pith yet.
Forward citations
Cited by 1 Pith paper
-
StarLoc: Pinpointing Transmitting LEO Satellites from a Single Passive Array
StarLoc achieves 3D localization of LEO transmitters to 0.7° angle accuracy and 5 km range using only three ground antennas by exploiting the 2D orbital motion manifold.
discussion (0)
Sign in with ORCID, Apple, or X to comment. Anyone can read and Pith papers without signing in.