Hybrid CubeSat constellation design for observing hurricanes
Abstract
State-of-the-art weather forecasting systems depend on various data collected by
airborne, orbiting, and ground sensors. Regional CubeSat constellations have the potential
to improve hurricane forecasting by collecting sensor data over data-starved oceanic
regions. Even in areas where terrestrial sensor networks exist, constellation sensor data can
help reduce forecasting model errors. To this end, we consider the problem of designing a
low-Earth orbit CubeSat constellation that meets resolution requirements over a region of
interest. Specifically, we envision a novel mission design concept referred to as a regional
hybrid constellation in which multiple formation-flying CubeSat clusters are deployed in a
traditional multi-plane constellation configuration.
To take advantage of the Repeating Ground Track (RGT) orbits within the regional
constellation, we present a new optimization-based approach to design an RGT orbit.
Using these RGT orbits in the constellation design can reduce the station-keeping cost of the
constellation. For the hybrid constellation, we design three novel formation designs that can
address the current observation gaps and improve hurricane forecast accuracy. We determine
the safe (no collision) relative orbits for each formation design. In addition, we consider a
novel optimization framework that utilizes satellite coverage maps to determine the number
of satellites and constellation patterns.
To facilitate the hybrid constellation design, we determine the CubeSat formation’s
coverage map analytically and use it within the optimization framework to determine
the optimal hybrid constellation design. Optimizing the hybrid constellation considers
minimizing the infrastructure and maintenance cost of the constellation while maximizing
the quantity and quality of the hurricane data collection. The hybrid constellation design
considers the second-order geo-potential perturbations such that there will be no coverage
degradation of the hybrid constellation over the region of interest under these perturbations.
Additionally, we develop control strategies for station-keeping and formation-keeping of the
hybrid constellation using chemical and electrical propulsion.
Description
Thesis (Ph.D.)-- Wichita State University, College of Engineering, Dept. of Aerospace Engineering