| タイトル | Development of ADOCS controllers and control laws. Volume 2: Literature review and preliminary analysis |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870008275 |
| 著者（英） | Landis, Kenneth H.; Glusman, Steven I. |
| 著者所属（英） | Army Research and Technology Labs.|Boeing Vertol Co. |
| 発行日 | 1985-03-01 |
| 言語 | eng |
| 内容記述 | The Advanced Cockpit Controls/Advanced Flight Control System (ACC/AFCS) study was conducted by the Boeing Vertol Company as part of the Army's Advanced Digital/Optical Control System (ADOCS) program. Specifically, the ACC/AFCS investigation was aimed at developing the flight control laws for the ADOCS demonstrator aircraft which will provide satisfactory handling qualities for an attack helicopter mission. The three major elements of design considered are as follows: Pilot's integrated Side-Stick Controller (SSC) -- Number of axes controlled; force/displacement characteristics; ergonomic design. Stability and Control Augmentation System (SCAS)--Digital flight control laws for the various mission phases; SCAS mode switching logic. Pilot's Displays--For night/adverse weather conditions, the dynamics of the superimposed symbology presented to the pilot in a format similar to the Advanced Attack Helicopter (AAH) Pilot Night Vision System (PNVS) for each mission phase as a function of ACAS characteristics; display mode switching logic. Findings from the literature review and the analysis and synthesis of desired control laws are reported in Volume 2. Conclusions drawn from pilot rating data and commentary were used to formulate recommendations for the ADOCS demonstrator flight control system design. The ACC/AFCS simulation data also provide an extensive data base to aid the development of advanced flight control system design for future V/STOL aircraft. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 87N17708
USAAVSCOM-TR-84-A-7-VOL-2
NAS 1.26:177339-VOL-2
NASA-CR-177339-VOL-2
D210-12323-VOL-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/151943 |
