Data-Driven and Dynamically Feasible Trajectory Generation for Real-Time Powered Descent Guidance and Robotic Exploration

Increasingly complex and high-mass planetary missions require autonomous long-horizon trajectory generation to achieve dynamically feasible powered descent guidance. While analytical and indirect methods are computationally efficient, significant simplifications of the dynamics and constraints are required for both problem formulations. Numerical optimization algorithms enable minimum-energy trajectory generation subject to system dynamics and safety constraints but currently remain computationally infeasible on flight-grade processors, taking seconds to minutes to compute a single trajectory. The objective of this dissertation is to develop new algorithms to advance the state of the art in trajectory optimization and planning for autonomous systems. Due to the limited computational abilities of radiation-hardened processors and an increased need for spacecraft and robotic autonomy, specialized algorithms capable of running in realtime constitute enabling technologies for space exploration. Three major contributions are developed in this dissertation. First, a transformer neural network-based algorithm is created to predict the tight constraints that recover the solution and parameter sets for constrained optimization problems. By training on prior runs of the numerical optimization solver, the learned mapping can construct a reduced problem formulation that recovers the optimal solution while reducing runtime by up to an order of magnitude. Second, a method to embed problem-specific information into the neural network training process was developed. By embedding the Lagrangian and Lagrangian gradient merit functions into the training process, neural network-generated control policies are biased toward constraint satisfaction. Third, an autonomous hybrid targeting and guidance algorithm was designed to utilize probabilistic risk maps and numerical optimization to select and navigate to minimum-risk landing sites. Applications in planetary powered descent and landing, as well as rover path planning, are used to benchmark algorithm performance.

Name thesis:degree_name

Doctoral

Department dc:contributor.department

Massachusetts Institute of Technology. Department of Aeronautics and Astronautics

Grantor dc:publisher

Massachusetts Institute of Technology

Year dc:date.issued

2024

Author dc:creator

• Briden, Julia

Advisors dc:contributor.advisor

• Linares, Richard
• Marzouk, Youssef
• Cauligi, Abhishek

Statement dc:rights

• In Copyright - Educational Use Permitted
• Copyright retained by author(s)

Licence dc:rights.uri

• https://rightsstatements.org/page/InC-EDU/1.0/

Handle dc:identifier.uri

https://hdl.handle.net/1721.1/163526

OAI identifier oai:identifier

oai:dspace.mit.edu:1721.1/163526