Advanced Space Concepts Laboratory · RPI
We develop rigorous analytical and computational frameworks for multi-body dynamical systems, enabling observer constellation design for space domain awareness (SDA), adversarial RSO tracking and maneuver detection, terrain-relative navigation, and autonomous guidance, navigation, and control (GN&C) for planetary landing and deep-space missions.
Research Focus
Cislunar SDA · AFOSR-funded
Submodular D-optimality optimization of lunar surface sensor placements for robust cislunar RSO custody. The framework integrates terrain-aware bright-body exclusion (Sun, Earth), IEKF-based FIM aggregation across full RSO catalogs, and a Greedy Sequential Differential Evolution (GSDE) optimizer for near-real-time placement decisions.
Key Capabilities
Submodular placement with Sun/Earth exclusion zones
D-optimality via log-det FIM maximization
IEKF tracking across full RSO catalog
Greedy Sequential Differential Evolution (GSDE)
Ground-track & 3D constellation visualization
CSV export of network performance metrics
Key Contributions
Node-removal sensitivity analysis across orbit families (L1/L2 Halo, NRHO, DRO)
FIM-based degradation curves quantifying coverage loss per node lost
Identification of critical vs. redundant constellation members
Attrition-resilience ranking across orbit family geometries
Adversarial SDA · Constellation Survivability
Quantifies how quickly a hostile actor can degrade a cislunar SDA constellation's tracking coverage through targeted removal or denial of individual observer nodes, across L1/L2 Halo, NRHO, and DRO periodic orbit families, establishing attrition-rate metrics for resilient constellation design under adversarial threat models.
Low-Thrust Trajectories · Probabilistic Reachability
Gaussian process surrogates accelerate low-thrust reconfiguration and transfers by learning the optimal cost landscape across periodic orbit families. Probabilistic reachability level sets rapidly quantify accessible destinations under navigation uncertainty without repeated TPBVP solves, while invariant-manifold-seeded ballistic terminal coast arcs reduce propellant requirements.
Key Contributions
GP surrogates with ARD kernels — NHL/SHL families
Probabilistic reachability under navigation error
Manifold-seeded TPBVP initialization
Ballistic terminal coast arc exploitation
Key Contributions
Classification of linear and non-linear quasi-periodic behavior
Formulation of OCP in torus space
Comparison of results with phase space TPBVP solutions
Rephasing for reconfiguration of space constellations
Astrodynamics · Invariant Tori · CR3BP
Expand reachability framework to leverage quasi-periodic invariant structures seeded from periodic orbits in the CR3BP. Develop cost functions that define novel and relevant metrics and compare solutions in torus and phase spaces.
Funding & Partnerships
Supported by federal agencies and industry partners advancing the cislunar mission.
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Get in Touch
Send all enquiries for research positions to sandes5@rpi.edu. Include your CV with education, past research/work experience and a list of references.
J. Erik Jonsson Engineering Center · RPI Campus · Troy, NY