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Title:
飛行体用航法装置および飛行体用航法
Document Type and Number:
Japanese Patent JP6628254
Kind Code:
B2
Abstract:
To provide a flight vehicle-purpose navigation device that can properly correct posture errors even when using a general-purpose inertial measurement device of low accuracy.SOLUTION: A flight vehicle-purpose navigation device, which is mounted to a fight vehicle, comprises: a detection device that detects inertia force acting on the flight vehicle; a first estimation unit that estimates a first error serving as at least a part of error ingredients between an initial setting posture of the detection device and a mounting posture relative to the flight vehicle on the basis of a result of a correction by gravity acceleration with respect to acceleration detected by the detection device when the flight vehicle stands still; and a positioning unit that derives a position and velocity of the flight vehicle on the basis of the initial setting posture in which the first error estimated by the first estimation unit is removed.SELECTED DRAWING: Figure 5

Inventors:
Yukiko Sunami
Mountain Saki Toshifumi
Satoshi Nakayama
Kazuaki Saito
Application Number:
JP2017069167A
Publication Date:
January 08, 2020
Filing Date:
March 30, 2017
Export Citation:
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Assignee:
Japan Aerospace Exploration Agency
Mitsubishi Precision Co., Ltd.
International Classes:
G01C15/00; B64G1/24; B64G1/36; G01S19/40; G01S19/47
Domestic Patent References:
JP2008304260A
JP2007121008A
JP3025315A
JP2008038418A
JP9261149A
Attorney, Agent or Firm:
Sumio Tanai
Hiroyuki Hashimoto
Hiroshi Yamaguchi
Takeo Okita
Norihiko Ara