Title:
垂直離着陸飛翔装置
Document Type and Number:
Japanese Patent JP4135736
Kind Code:
B2
Abstract:
A vertical takeoff and landing aircraft according to the invention includes multiple thrust producing devices that produce thrusts applied in the substantially vertically upward direction; a target attitude setting portion that sets a target attitude used in attitude control of the aircraft; an inertia moment deriving portion that derives an inertia moment applied around a predetermined rotational axis of the aircraft; and a thrust adjustment portion that adjusts, during the attitude control of the aircraft, the thrusts to be produced by the respective thrust producing devices based on the target attitude set by the target attitude setting portion and the inertia moment during the attitude control, which is derived by the inertia moment deriving portion.
Inventors:
Ishiba Masatsugu
Application Number:
JP2005241479A
Publication Date:
August 20, 2008
Filing Date:
August 23, 2005
Export Citation:
Assignee:
TOYOTA JIDOSHA KABUSHIKI KAISHA
International Classes:
B64C29/00
Domestic Patent References:
| JP2005125976A | ||||
| JP2005053279A | ||||
| JP2003252298A | ||||
| JP5119837A | ||||
| JP3206473B2 | ||||
| JP2620428B2 | ||||
| JP7047399B2 |
Attorney, Agent or Firm:
Yoshiyuki Kawaguchi
Hidemi Matsukura
Mayuko Wakuda
Kazunobu Sera
Tsutomu Toyama
Hidemi Matsukura
Mayuko Wakuda
Kazunobu Sera
Tsutomu Toyama
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