Implementation of a Six Degree of Freedom Precision Lunar Landing Algorithm Using Dual Quaternion RepresentationIn this study, a powered descent guidance algorithm using a unit dual quaternion represen- tation of the vehicle dynamics is implemented in a high-fidelity simulation and on representative flight hardware. This Dual-Quaternion Guidance (DQG) algorithm is applied to the precision lunar landing problem which levies complex constraints upon the trajectory, including state triggered attitude constraints to enable terrain-relative navigation and hazard detection as well as real-time requirements for landing site re-designation. The investigation explores DQG’s usefulness as a mission design tool as well as a real-time guidance algorithm and defines real-time performance requirements for the hazard detection and avoidance (HDA) re-targeting phase of precision lunar landing. The experiment is presented in two parts. First, DQG is implemented within a high-fidelity Monte Carlo simulation to tune the algorithm’s parameters for the simulated vehicle, to refine the mission design, and to develop guidance update timing requirements to perform the HDA maneuver. DQG generates trajectories online for the divert which are tracked by the vehicle’s inner-loop controllers to the targeted landing site. Second, DQG is run on representative hardware to demonstrate real-time operation through a divert maneuver. These results allow for rapid, flexible, optimal mission design satisfying complex constraints, and for the definition of real-time performance requirements for the HDA operations inherent in precision lunar landing. The HDA divert maneuver is found to require guidance trajectory updates in less than three seconds. DQG is found to be too slow to meet this update timing on the descent and landing computer (DLC) in its current implementation. DQG running on alternative hardware can meet the update rate requirement. Algorithm implementation improvements are also recommended which are expected to speed up computation sufficiently to meet requirements on the DLC.
Document ID
20210024113
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Lloyd D Strohl III (Blue Origin Kent, Washington, United States)
Andrew W. Berning, Jr (Blue Origin Kent, Washington, United States)
Stefan Bieniawski (Blue Origin Kent, Washington, United States)
Javier A Doll (Draper Laboratory Cambridge, Massachusetts, United States)
Matthew P Fritz (Draper Laboratory Cambridge, Massachusetts, United States)
Stephanie White (Odyssey Space Research (United States) Houston, Texas, United States)
John M Carson (Johnson Space Center Houston, Texas, United States)
Behcet Acikmese (Johnson Space Center Houston, Texas, United States)
Date Acquired
November 8, 2021
Subject Category
Spacecraft Instrumentation And Astrionics
Meeting Information
Meeting: AIAA SciTech Forum
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics