Research

My current and past research topics

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Projects

A selection of projects I have worked on

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Blog

Exploring a nonlinear world one assumption at a time

Minimum Periapse for a Gravity Assist

TLDR: 100 km above the atmosphere Gravity assists are an astrodynamics maneuver to steal a small amount of a planet’s angular momentum to give your spacecraft a much more significant boost. Exactly how much momentum you can steal is defined by the arrival velocity vector relative to the planet and the maximum turning angle you…

Measuring Resilience Of Autonomous Controllers To Missed Thrust Events – ESA GNC – 2021

Note: This post is adapted from my conference paper, which was presented at the 11th International ESA Conference on Guidance, Navigation & Control Systems. You can read the full paper here. Abstract – Measuring Resilience Of Autonomous Controllers To Missed Thrust Events On A Mars To Earth Trajectory As spacecraft adopt low-thrust electric propulsion to reduce propellant mass,…

Adding Non-Standard Bodies to SPICE using Horizons

In astrodynamics, when you need high-quality Ephemeris data for some celestial body, you generally turn to NASA’s NAIF’s (Navigation and Ancillary Information Facility) SPICE toolkit. Because the setup of SPICE with non-standard bodies is a one-off step and usually the first step in several of my projects, it’s something I only do a handful of…

Designing Trajectories Resilient to Missed Thrust Events Using Expected Thrust Fraction – Aerospace Science and Technology

Note: This post is adapted from my journal paper, which was accepted to Aerospace Science and Technology in Spring 2021. You can read the full paper here Abstract – Designing Trajectories Resilient to Missed Thrust Events Using Expected Thrust Fraction With the adoption of efficient low-thrust propulsion methods, the probability of a missed thrust event…

Expected Thrust Fraction: Resilient Trajectory Design Applied to the Earth Return Orbiter – AAS/AIAA SFMC- 2021

Note: This post is adapted from my conference paper, which was presented at the Space Flight Mechanics Conference in Winter 2021. You can read the full paper here. Abstract – Expected Thrust Fraction: Resilient Trajectory Design Applied to the Earth Return Orbiter Electric propulsion is an enabling technology for NASA’s Mars Sample Return mission that affords an…

Designing Trajectories Resilient to Missed Thrust Events Using Expected Thrust Fraction – ASC- 2020

Note: This post is adapted from my conference paper, which was presented at the Astrodynamics Specialists Conference in Summer 2020. You can read the full paper here. Abstract – Designing Trajectories Resilient to Missed Thrust Events Using Expected Thrust Fraction With the adoption of efficient low-thrust propulsion methods, the probability of a missed thrust event occurring has…

Using Reinforcement Learning to Design Missed Thrust Resilient Trajectories – ASC- 2020

Note: This post is adapted from my conference paper, that I presented at the Astrodynamics Specialists Conference in Summer 2020. You can read the full paper here. Abstract – Using Reinforcement Learning to Design Missed Thrust Resilient Trajectories From ion thrusters to solar sails, spacecraft continue to adopt new and more efficient forms of propulsion. As…

Neural Network Optimal Control in Astrodynamics: Application to the Missed Thrust Problem – Acta Astronautica

Note: This post is adapted from my journal paper, which was accepted to Acta Astronautica in Spring 2020. You can read the full paper here Abstract – Neural Network Optimal Control in Astrodynamics While high-efficiency propulsion techniques are enabling new mission concepts in deep space exploration, their limited thrust capabilities necessitate long thrusting arcs and…