Manual Attitude Control Systems
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Manual Attitude Control Systems
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Author : Robert O. Besco
language : en
Publisher:
Release Date : 1964
Manual Attitude Control Systems written by Robert O. Besco and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Flight control categories.
Manual Attitude Control Systems
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Author : R. O. Besco
language : en
Publisher:
Release Date : 1963
Manual Attitude Control Systems written by R. O. Besco and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Flight control categories.
Manual Attitude Control Systems Parametric And Comparative Studies Of Operating Modes Of Control
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Author : D. K. Bauerschmidt
language : en
Publisher:
Release Date : 1964
Manual Attitude Control Systems Parametric And Comparative Studies Of Operating Modes Of Control written by D. K. Bauerschmidt and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
Operation And Service Manual For Attitude Control System Electronics Efc Console 52e270002
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Author : MCDONNELL DOUGLAS ASTRONAUTICS CO ST LOUIS MO.
language : en
Publisher:
Release Date : 1968
Operation And Service Manual For Attitude Control System Electronics Efc Console 52e270002 written by MCDONNELL DOUGLAS ASTRONAUTICS CO ST LOUIS MO. and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
The purpose of the Space Technical Data Report (STDR) is to familiarize personnel with the operation and service of the Attitude Control System Electronics (ACSE) Equipment Functional Check (EFC) Console, 52E270002. The STDR describes the console, associated panels and their functions. The console is used in conjunction with related Aerospace Ground Equipment to perform EFC procedures on the Attitude Control Electronics Group and Pad Abort Thruster Electronics. (Author).
Simulator Studies Of The Manual Control Of Vehicle Attitude Using An On Off Reaction Control System
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Author : Armando E. Lopez
language : en
Publisher:
Release Date : 1963
Simulator Studies Of The Manual Control Of Vehicle Attitude Using An On Off Reaction Control System written by Armando E. Lopez and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Elevators (Airplanes) categories.
Manual Attitude Control Systems
DOWNLOAD
Author : Robert O. Besco
language : en
Publisher:
Release Date : 1964
Manual Attitude Control Systems written by Robert O. Besco and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Flight control categories.
Simulator Studies Of The Manual Control Of Vehicle Attitude Using An On Off Reaction Control System
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Author : Armando E. Lopez
language : en
Publisher:
Release Date : 1963
Simulator Studies Of The Manual Control Of Vehicle Attitude Using An On Off Reaction Control System written by Armando E. Lopez and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Elevators (Airplanes) categories.
Vector Reticle Control Action Display In Manual Control Of Space Vehicle Attitude
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Author : Robert H Cannon (Jr)
language : en
Publisher:
Release Date : 1964
Vector Reticle Control Action Display In Manual Control Of Space Vehicle Attitude written by Robert H Cannon (Jr) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
Two concepts, the vector reticle and control action display, are submitted as effective means for making manual threeaxis attitude control quicker and more efficient while reducing substantially the concentration required of the pilot. A system design is submitted in which the two concepts are combined in a control action reticle and in which the pilot has direct control of the jet valves. (The entire system may be mechanical.) The system is controlled to a visual reference or to an instrument attitude reference. Malfunction of the system cannot interfere with normal manual control. The vector recticle presents all auxiliary information in a single three-part geometric vector superimposed on the window (rather than on three separate dials, for example), thus reducing the number of quantities to be monitored from three to one. Control action display gives the pilot instantaneous and exclusive control of the reticle, thus removing the need for two mental integrations and greatly reducing the concentration required for tracking. Results are presented of three-axis (fixed-base) simulation studies of the proposed system and of other systems for comparison. (Author).
A Study Of Fully Manual And Augmented Manual Control Systems For The Saturn 5 Booster Using Analytical Pilot Models
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Author :
language : en
Publisher:
Release Date : 1968
A Study Of Fully Manual And Augmented Manual Control Systems For The Saturn 5 Booster Using Analytical Pilot Models written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
Guidance And Control Mechanics Test Attitude Control System Analytical Performance Verification
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Author : MCDONNELL CO ST LOUIS MO.
language : en
Publisher:
Release Date : 1968
Guidance And Control Mechanics Test Attitude Control System Analytical Performance Verification written by MCDONNELL CO ST LOUIS MO. and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.
Closed-loop attitude control system analytical performance verification tests were conducted for the Gemini B spacecraft and the mated Gemini B-Manned Orbiting Laboratory (MOL) configurations. Both manual and automatic modes were tested. The primary concern was the ability to control and display accurately attitude and rates of the Gemini B spacecraft. Tests of the inertial platform were performed on a 3-Axis Flight Motion Simulator, driven by an analog computer. The analog computer also mechanized the dynamic equations of motion for both configurations. (Author).