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Engineering portfolio
Browse nine aerospace projects with concise scope, evidence classification and links to detailed work or public source.
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Open a case study for methods and plots, or go directly to public source where it exists.
Target estimation through camera dropouts using an IMM pipeline, deterministic analytic truth tests and Raspberry Pi execution data.
Evidence boundary: Hardware trials show directional and dropout behavior, not independent metrology truth; the public timing result also misses its target.
C++ flight-software baseline with command handling, mode logic, FDIR, deterministic fault campaigns and an interactive browser model.
Evidence boundary: Raspberry Pi execution demonstrates portability, not hard-real-time qualification.
Synthetic aircraft-fitting substantiation covering classical margins, finite-element response, tolerance effects and adverse statistical cases.
Evidence boundary: Educational, synthetic and non-OEM; this is not approved aircraft stress substantiation.
Autopilot testing against actuator limits, gusts and model uncertainty, including a seeded 50-run campaign.
Evidence boundary: Uses a low-order representative model; it is not validated F-16 flight dynamics.
Early point-mass landing simulation used to define the next modeling and verification gates.
Evidence boundary: Current source supports one representative run, not a statistical landing campaign.
Requirements, engineering-change, thermal and review support for a student spacecraft payload program.
Evidence boundary: Program artifacts are limited and the role cannot be independently verified from public source.
Perception-to-actuation prototype organized around a measurable latency budget.
Evidence boundary: Source code and raw timing logs are not public, so exact performance is reported rather than independently verified.
Precision-landing UAV concept retained as an engineering design-review closeout.
Evidence boundary: The project ended at design review; no flight campaign was completed.
Public relative-navigation reference implementation with geometry, a 12-state UKF, FDIR and replay scaffolding.
Evidence boundary: No hardware campaign or validated accuracy, timing or flight-readiness result exists yet.