2010 Fiscal Year Final Research Report
Design of Guidance and Control System for Manned Spaceplane Accommodating Variation in Dynamic Characteristics and Failure
| Project/Area Number |
20560740
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Nihon University |
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Principal Investigator |
SHIMADA Yuzo Nihon University, 理工学部, 教授 (90060235)
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| Co-Investigator(Renkei-kenkyūsha) |
ABE Akio 日本大学, 理工学部, 助教 (60434114)
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| Project Period (FY) |
2008 – 2010
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| Keywords | 宇宙往還機 / 有人宇宙輸送システム / 回収技術 / 飛行制御 / 適応制御 / 耐故障制御 / 外乱オブザーバ / フィードバック線形化 |
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| Research Abstract |
Two types of adaptive control law were studied with the aim of improving the reliability of manned space transportation. One is a novel nonparametric approach and the other is a conventional parametric approach. On the basis of the first approach, a flight control system was designed by combining disturbance observers and a feedback linearization technique. A numerically simulated automatic landing on a runway was successfully carried out using the data of a space shuttle orbiter. In the second method, lateral directional motion was adapted to design a minimum phase system, and its effectiveness was confirmed by numerical simulation with a disturbance observer. A fault-tolerant control law was also developed so that a flight performance can be maintained, even if one or two actuators among the five control surfaces break down.
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