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Extending Explicit Guidance Methods to Higher Dimensions, Additional Conditions, and Higher Order IntegrationGuidance functions play critical roles in autonomy to steer vehicles and aircraft to the intended target or destination. Explicit guidance (E Guidance) solves the two-point boundary value problem with initial and final conditions for position and velocity. The original formulation of E Guidance involves translational acceleration commands with a direct relationship to time, and it is possible to modify E Guidance for rotational acceleration. Other extensions for E Guidance include higher dimensions, additional conditions, and higher-order integration of the linearly independent E Guidance functions. The most promising extension involves higher-order integration of the E Guidance functions, but it may be physically impractical by initially moving away from the target. This paper provides a brief overview of some methods that extend E Guidance to higher dimensions, utilize additional conditions, or perform higher-order integration, and if they satisfy the two-point boundary value problem.
Document ID
20230003045
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Evan Kawamura
(Ames Research Center Mountain View, California, United States)
Dilmurat Azimov
(University of Hawaii at Manoa Honolulu, Hawaii, United States)
Date Acquired
March 7, 2023
Subject Category
Aeronautics (General)
Spacecraft Design, Testing and Performance
Astronautics (General)
Meeting Information
Meeting: IUTAM Symposium on Optimal Guidance and Control for Autonomous Systems
Location: Honolulu, HI
Country: US
Start Date: March 15, 2023
End Date: March 17, 2023
Sponsors: University of Hawaii at Manoa
Funding Number(s)
WBS: 109492.02.01.07.07
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
explicit guidance
polynomials
unmanned aerial vehicles
boundary conditions
higher-order integration
additional conditions
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