People
Ye Lu, Ph.D.
Ye Lu leads LSPE and studies astrodynamics, atmospheric flight mechanics, mission design, and guidance, navigation, and control for future space exploration missions.
Ye Lu is an Assistant Professor in the Aerospace Engineering Department at Worcester Polytechnic Institute and leads the Laboratory for Spaceflight and Planetary Exploration. His research focuses on astrodynamics, atmospheric flight mechanics, mission design, and guidance, navigation, and control technologies for future space exploration missions.
Before joining WPI, he was an Assistant Professor at Kent State University from 2019 to 2023.
Research Areas
Astrodynamics
Hypersonic Flight Mechanics
Guidance, Navigation, and Control
Education
Ph.D. Aeronautics and Astronautics, Purdue University, 2019
M.S. Aerospace Engineering, Worcester Polytechnic Institute, 2015
B.S. Aerospace Engineering & Mathematical Sciences (Double Major), Worcester Polytechnic Institute, 2013
Publications
Teaching
AE 2320 Undergraduate Introduction to Orbital Mechanics
Course description
An introductory course that covers the fundamentals of space flight. Topics studied include: two-body orbital dynamics, classification of orbits, and time of flight analysis; geocentric orbits and impulsive maneuvers: orbit shaping, escape trajectories, Hohmann and non-Hohmann transfers; orbital elements in 3D; interplanetary Hohmann and generalized transfers, intercepts, flybys.
AE 3310 Undergraduate Fundamentals of Navigation and Communications
Course description
This course covers methods and current technologies in the analysis, synthesis, and practice of aerospace guidance, navigation, and communications systems. Topics covered include: attitude- and position kinematics, inertial navigation systems, global satellite navigation systems, communication architectures for satellite navigation, satellite link performance parameters and design considerations, tropospheric and ionospheric effects on radio-wave propagation, least squares estimation, and the Kalman filter.
AE 5336/5093 Graduate Orbital Mechanics
Course description
The course covers the natural dynamics of objects under gravity, including orbits in the two-body problem and the three-body problem. Fundamental techniques for astrodynamics cover Lagrange functions, Lambert's theorem, and patched conics. Application in trajectory design include orbital maneuvers/transfer and interplanetary orbits. Mission design software will be used to model orbit and trajectory.
MQP
Small Spacecraft Explores Neptune without RPS
Abstract
Available Soon
Conceptual Mission Design for Titan Sample Return
Won Provost MQP Award
Abstract
Saturn’s moon Titan is a prime target for exploration due to its dense nitrogen-rich atmosphere and carbon-containing molecules, suggesting possible life. Beyond Cassini/Huygens, exploration has been minimal, but NASA’s Dragonfly mission (2028) will study Titan’s surface. The proposed mission aims to return 30 samples from Selk Crater. Utilizing NASA’s ISRU concept for return propellant, key considerations included trajectory, communication, ADCS, EDL, sample collection, and power.
A planned 2051 launch with gravity assists leads to a 19-year total mission length. On the surface, a quadcopter will collect samples, and an ISRU plant will produce fuel for return. Thermal isolation and liquid oxygen will maintain sample integrity of the samples during the return to Earth.
Design and Analysis of a SmallSat as a Communication Relay for Venus Atmospheric Probes
Abstract
This paper discusses a conceptual mission to Venus which utilizes the Lofted Environmental and Atmospheric Venus Sensors (LEAVES) to investigate the sulfur cycle and the unknown compound that absorbs near-ultraviolet light in the atmosphere. The mission uses two separate spacecraft coupled at launch, an autonomous bus, Demeter, carrying 144 LEAVES probes and a communications orbiter, Persephone, to relay data from the LEAVES to Earth.
The LEAVES are estimated to be at a Technology Readiness Level (TRL) of 3, while the spacecraft consists of parts at TRL 9. The unique launch mechanism for the LEAVES is at a TRL of 1-2, and the mission meets the Concept Maturity Level (CML) requirements for a CML 4 classification.