Gravity turn ascent profile optimization with a staged delta-v budget model.
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Updated
Jul 31, 2026 - Python
Gravity turn ascent profile optimization with a staged delta-v budget model.
Core principles and mathematical models for rocketry and orbital mechanics, implemented in code.
Delta-v planner for circular-to-circular transfers (Hohmann, bi-elliptic, plane-change). Impulsive burns, quick trade-offs. Python 3.10+.
Systems-level quantitative feasibility study of Mars colonization under strict scientific and engineering constraints.
Interactive Python tool that computes asteroid rendezvous launch windows using Lambert transfers, Earth ephemerides, and user-defined orbital elements.
v2.6 refines 3I/ATLAS analysis with automated peak detection, improved Δv modelling, Ni/Fe compositional anomaly, colour–brightness evolution, and multi-station validation of post-perihelion noise events.
Python-based orbital mission planner for realistic spaceflight and orbital mechanics calculations (KSP-RSS-Principia inspired)
Pure Standard ML orbital mechanics: vis-viva, circular/escape velocity, Hohmann and bi-elliptic transfers, Tsiolkovsky rocket equation, sphere of influence (MLton + Poly/ML)
Minimum-Δv impulsive maneuver planning for spacecraft relative orbits - a finite-difference-verified Rust port of the Koenig & D'Amico (IEEE TAC 2020) fuel-optimal impulsive control algorithm.
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