書誌事項
- タイトル別名
-
- On the Design of an Adaptive Observer and its Application to VTOL Flight Control System
- アダプティブ オブザーバ セッケイ ト ソノ VTOLキ ヒコウ セイギョケイ
この論文をさがす
抄録
The subject of modern control theory has received increased interest in recent years, partly because of its importance as an analytical tool for the study of advanced control technology such as CCV, and of the corresponding active control approaches. However, the main disadvantage of the modern control technique is its dependence on the accessibility of all the state variables and parameters of the plant to be controlled or identified. In this report, an adaptive observer scheme is developed to estimate the state vector and to identify all the parameters of a single-input single-output n-th order linear system where only the input and output can be observed, and is based on the new canonical form method without LIAPUNOV'S direct method. The approach is proved to be asymptotically stable and thus ensuring the convergence of the identification algorithm.<BR>Numerical computations are done for the parameter identification and state estimation problems of VTOL aircraft and for the synthesis of a state feedback controller.
収録刊行物
-
- 日本航空宇宙学会誌
-
日本航空宇宙学会誌 25 (285), 494-501, 1977
一般社団法人 日本航空宇宙学会
- Tweet
詳細情報 詳細情報について
-
- CRID
- 1390001204506499840
-
- NII論文ID
- 130003958203
-
- NII書誌ID
- AN00189072
-
- ISSN
- 24241369
- 00214663
-
- NDL書誌ID
- 1849735
-
- 本文言語コード
- ja
-
- データソース種別
-
- JaLC
- NDL
- Crossref
- CiNii Articles
-
- 抄録ライセンスフラグ
- 使用不可