Redesign of a Variable-Gain Output Feedback Longitudinal Controller Flown on the High-Alpha Research Vehicle (Harv)

Redesign of a Variable-Gain Output Feedback Longitudinal Controller Flown on the High-Alpha Research Vehicle (Harv)
Author :
Publisher : Createspace Independent Publishing Platform
Total Pages : 36
Release :
ISBN-13 : 1722725656
ISBN-10 : 9781722725655
Rating : 4/5 (55 Downloads)

Book Synopsis Redesign of a Variable-Gain Output Feedback Longitudinal Controller Flown on the High-Alpha Research Vehicle (Harv) by : National Aeronautics and Space Administration (NASA)

Download or read book Redesign of a Variable-Gain Output Feedback Longitudinal Controller Flown on the High-Alpha Research Vehicle (Harv) written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-10 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehicle (HARV) during calendar years (CY) 1995 and 1996. Linear models are developed for both the modified controller and a baseline controller that was flown in CY 1994. The modified controller was developed with three gain sets for flight evaluation, and several linear analysis results are shown comparing the gain sets. A Neal-Smith flying qualities analysis shows that performance for the low- and medium-gain sets is near the level 1 boundary, depending upon the bandwidth assumed, whereas the high-gain set indicates a sensitivity problem. A newly developed high-alpha Bode envelope criterion indicates that the control system gains may be slightly high, even for the low-gain set. A large motion-base simulator in the United Kingdom was used to evaluate the various controllers. Desired performance, which appeared to be satisfactory for flight, was generally met with both the low- and medium-gain sets. Both the high-gain set and the baseline controller were very sensitive, and it was easy to generate pilot-induced oscillation (PIO) in some of the target-tracking maneuvers. Flight target-tracking results varied from level 1 to level 3 and from no sensitivity to PIO. These results were related to pilot technique and whether actuator rate saturation was encountered. Ostroff, Aaron J. Langley Research Center RTOP 522-22-21-03...


Redesign of a Variable-Gain Output Feedback Longitudinal Controller Flown on the High-Alpha Research Vehicle (Harv) Related Books

Redesign of a Variable-Gain Output Feedback Longitudinal Controller Flown on the High-Alpha Research Vehicle (Harv)
Language: en
Pages: 36
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-10 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehicle (HARV) during calendar years (CY) 1995 and 1996. Linear m
Redesign of a Variable-gain Output Feedback Longitudinal Controller Flown on the High-Alpha Research Vehicle (HARV)
Language: en
Pages: 40
Authors: Aaron J. Ostroff
Categories: Feedback control systems
Type: BOOK - Published: 1998 - Publisher:

DOWNLOAD EBOOK

This paper describes a redesigned longitudinal controller that flew on the High-Alpha Research Vehicle (HARV) during calendar years (CY) 1995 and 1996. Linear m
High-Alpha Research Vehicle (HARV) Longitudinal Controller: Design, Analyses, and Simulation Resultss
Language: en
Pages: 68
High-Alpha Research Vehicle (Harv) Longitudinal Controller
Language: en
Pages: 64
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-08 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

This paper describes the design, analysis, and nonlinear simulation results (batch and piloted) for a longitudinal controller which is scheduled to be flight-te
Application of Variable-Gain Output Feedback for High-Alpha Control
Language: en
Pages: 30
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-08-17 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

A variable-gain, optimal, discrete, output feedback design approach that is applied to a nonlinear flight regime is described. The flight regime covers a wide a