Date of Award
3-2023
Document Type
Thesis
Degree Name
Master of Science
Department
Department of Aeronautics and Astronautics
First Advisor
Donald L. Kunz, PhD
Abstract
Recent research has been conducted in using deep reinforcement learning algorithms to generate closed form optimal control laws for helicopters in power loss scenarios. The control laws could allow for design of various cockpit visual pilot aids if proven successful. Such pilot aids are predicted to reduce pilot workload during execution of an emergency powerless landing, and to overall increase the probability of landing safely in such an event. The proposed topic discusses the use of the PPO algorithm in order to find an optimal control policy for a helicopter in a total power loss emergency landing scenario. The task consists of designing and training an actor neural network and a critic neural network using the PPO algorithm, along with developing the dynamic equations of motion for the helicopter, defining a reward structure and tweaking relevant hyper-parameters. The PPO algorithm has been proven overall feasible for bringing a simplistically modeled helicopter to safe landings over a wide range of initial flight conditions.
AFIT Designator
AFIT-ENY-MS-23-M-267
Recommended Citation
Eliash, Eidahn, "Estimation of Optimal Flight Trajectory in a Total Power Loss Scenario Using Proximal Policy Optimization" (2023). Theses and Dissertations. 7019.
https://scholar.afit.edu/etd/7019
Comments
A 12-month embargo was observed.
Approved for public release. Case number on file.