Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 302
Book Description
Accelerated Development and Flight Evaluation of Active Controls Concepts for Subsonic Transport Aircraft. Volume 1: Load Alleviation/extended Span Development and Flight Tests
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 302
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 302
Book Description
Accelerated Development and Flight Evaluation of Active Controls Concepts for Subsonic Transport Aircraft
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
Accelerated Development and Flight Evaluation of Active Controls Concepts for Subsonic Transport Aircraft. Volume 2: AFT C.G. Simulation and Analysis
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Book Description
NASA Reference Publication
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 770
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 770
Book Description
Integrated Application of Active Controls (IACC) Technology to an Advanced Subsonic Transport
Author: Boeing Commercial Airplane Company
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50
Book Description
Development and Flight Evaluation of an Augmented Stability Active Controls Concept
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723455742
Category :
Languages : en
Pages : 24
Book Description
A pitch active control system (PACS) was developed and flight tested on a wide body jet transport (L-1011) with a flying horizontal stabilizer. Two dual channel digital computers and the associated software provide command signals to a dual channel series servo which controls the stabilizer power actuators. Input sensor signals to the computer are pitch rate, column trim position, and dynamic pressure. Control laws are given for the PACS and the system architecture is defined. Discussions are given regarding piloted flight simulation and vehicle system simulation and vehicle system simulation tests that are performed to verify control laws and system operation prior to installation on the aircraft. Modifications to the basic aircraft included installation of the PACS, addition of a c.g. management system to provide a c.g. range from 25 to 39% mac, and downrigging of the geared elevator to provide the required nose down control authority for aft c.g. flight test conditions. Three pilots used the Cooper-Harper Rating Scale to judge flying qualities of the aircraft with PACS on and off. The handling qualities with the c.g. at 39% mac (41% stability margin) and PACS operating were judged to be as good as the handling qualities with the c.g. at 25% mac (+15% stability margin) and PACS off. Guinn, W. A. Unspecified Center NASA-CR-166009, NAS 1.26:166009, LR-30208-1 NAS1-15326
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723455742
Category :
Languages : en
Pages : 24
Book Description
A pitch active control system (PACS) was developed and flight tested on a wide body jet transport (L-1011) with a flying horizontal stabilizer. Two dual channel digital computers and the associated software provide command signals to a dual channel series servo which controls the stabilizer power actuators. Input sensor signals to the computer are pitch rate, column trim position, and dynamic pressure. Control laws are given for the PACS and the system architecture is defined. Discussions are given regarding piloted flight simulation and vehicle system simulation and vehicle system simulation tests that are performed to verify control laws and system operation prior to installation on the aircraft. Modifications to the basic aircraft included installation of the PACS, addition of a c.g. management system to provide a c.g. range from 25 to 39% mac, and downrigging of the geared elevator to provide the required nose down control authority for aft c.g. flight test conditions. Three pilots used the Cooper-Harper Rating Scale to judge flying qualities of the aircraft with PACS on and off. The handling qualities with the c.g. at 39% mac (41% stability margin) and PACS operating were judged to be as good as the handling qualities with the c.g. at 25% mac (+15% stability margin) and PACS off. Guinn, W. A. Unspecified Center NASA-CR-166009, NAS 1.26:166009, LR-30208-1 NAS1-15326
Development and Flight Evaluation of an Augmented Stability Active Controls Concept with a Small Tail
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 118
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 118
Book Description
Energy Research Abstracts
Author:
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 756
Book Description
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 756
Book Description
Advanced Control Technology and Its Potential for Future Transport Aircraft
Author: Hugh L. Dryden Flight Research Center
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 1066
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 1066
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.