AUTONOMOUS FORMATION FLYING IN LOW EARTH ORBIT
Dissertation Abstract: Formation flying is commonly identified as the collective usage of two or more cooperative spacecraft to exercise the function of a single monolithic virtual instrument. The distribution of tasks and payloads among fleets of coordinated smaller satellites offers the possibility to overcome the classical limitations of traditional single-satellite systems. The science return is enhanced through observations made with larger, configurable baselines and an improved degree of redundancy can be achieved in the event of failures. Different classes of formation flying missions are currently under discussion within the engineering and science community: technology demonstration missions, synthetic aperture interferometers and gravimeters for Earth observation, multi-spacecraft interferometers in the infrared and visible wavelength regions as a key to new astrophysics discoveries and to the direct search for terrestrial exoplanets. These missions are characterized by different levels of complexity, mainly dictated by the payload metrology and actuation needs, and require a high level of on-board autonomy to satisfy the continuously increasing demand of relative navigation and control accuracy.
This dissertation presents the first realistic demonstration of a complete guidance, navigation, and control (GNC) system for formation flying spacecraft in low Earth orbit. Numerous technical contributions have been made during the course of this research in the areas of formation flying guidance, GPS-based relative navigation, and impulsive relative orbit control, but the primary contribution of this thesis does not lie in one or more of these disciplines. The innovation and originality of this work stems from the design and implementation of a comprehensive formation flying system through the successful integration of various techniques. This research has led to the full development, testing and validation of the GNC flight code to be embedded in the on-board computer of the active spacecraft of the PRISMA technology demonstration. Furthermore key guidance and control algorithms presented here are going to be demonstrated for the first time in the TanDEM-X formation flying mission. Overall this thesis focuses on realistic application cases closely related to upcoming missions. The intention is to realize a practical and reliable way to formation flying: a technology that is discussed and studied since decades, but is still confined in research laboratories. Hardware-in-the-loop real-time simulations including a representative flight computer and the GPS hardware architecture show that simple techniques, which exploit the natural orbit motion to full extent, can meet the demanding requirements of long-term close formation-flying.
Author Biosketch: Simone D’Amico is an Assistant Professor of Aeronautics and Astronautics at Stanford University, a Terman Faculty Fellow of the School of Engineering, Founder and Director of the Space Rendezvous Laboratory, and Satellite Advisor of the Student Space Initiative, Stanford’s largest undergraduate organization. He received his B.S. and M.S. from Politecnico di Milano, and his Ph.D. from the Technical University of Delft. Before Stanford, Dr. D’Amico was at the German Aerospace Center (DLR) where he gave key contributions to the design, development, and operations of spacecraft formation-flying and rendezvous missions such as GRACE (USA/Germany), TanDEM-X (Germany), and PRISMA (Sweden/Germany/France) for which he received several awards. Dr. D’Amico’s research lies at the intersection of advanced astrodynamics, GN&C, and space system engineering to enable future distributed space systems. He has over 100 scientific publications including conference proceedings, peer-reviewed journal articles, and book chapters. He has been Programme Committee Member (2008), Co-Chair (2011), and Chair (2013) of the International Symposium on Spacecraft Formation Flying Missions and Technologies. He is Programme Committee Member of the International Workshop on Satellite Constellations and Formation Flying since 2013. D’Amico is Associate Editor of the Journal of Guidance, Control, and Dynamics and the Journal of Space Science and Engineering.
Author Contact: Simone D’Amico, Stanford University | Correspondence Address, Department of Aeronautics and Astronautics, Durand Building, 496 Lomita Mall, Stanford, CA 94305 USA | Phone: (650) 497-4682 | Email: email@example.com