A fuzzy logic based spacecraft controller for six degree of freedom control and performance resultsThe development philosophy of the fuzzy logic controller is explained, details of the rules and membership functions used are given, and the early results of testing of the control system for a representative range of scenarios are reported. The fuzzy attitude controller was found capable of performing all rotational maneuvers, including rate hold and rate maneuvers. It handles all orbital perturbations very efficiently and is very responsive in correcting errors.
Document ID
19910065121
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lea, Robert N. (NASA Johnson Space Center Houston, TX, United States)
Hoblit, Jeffrey (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Jani, Yashvant (LinCom Corp. Houston, TX, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 91-2800
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference