@inproceedings{41d1032778dc46b28b0932c5c477d655,
title = "Further evaluation of an adaptive method for launch vehicle flight control",
abstract = "Future reusable launch vehicles must be designed to fly a wide spectrum of missions and survive numerous types of failures. The X-33 Reusable Launch Vehicle Technology Demonstrator is used as a simulation platform for testing a neural network-based model-reference adaptive controller and comparing it to a gain scheduled controller in the case of a mission undergoing an engine-out abort scenario. The adaptive controller is able to perform nearly as well as a gain-scheduled controller, and suggestions are made for further improvements.",
author = "Johnson, {Matthew D.} and Cause, {Anthony J.} and Johnson, {Eric N.}",
year = "2004",
doi = "10.2514/6.2004-5016",
language = "English (US)",
isbn = "1563476703",
series = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "1354--1370",
booktitle = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference",
note = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference ; Conference date: 16-08-2004 Through 19-08-2004",
}