Attitude Determination Algorithm Based on Antenna Configuration

CUI Jianhua; CHENG Naiping

doi:10.11999/JEIT160347

Volume 39 Issue 2

Feb. 2017

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Article Navigation > Journal of Electronics & Information Technology > 2017 > 39(2): 459-465

CUI Jianhua, CHENG Naiping. Attitude Determination Algorithm Based on Antenna Configuration[J]. Journal of Electronics & Information Technology, 2017, 39(2): 459-465. doi: 10.11999/JEIT160347

Citation:

CUI Jianhua, CHENG Naiping. Attitude Determination Algorithm Based on Antenna Configuration[J]. Journal of Electronics & Information Technology, 2017, 39(2): 459-465. doi: 10.11999/JEIT160347

CUI Jianhua, CHENG Naiping. Attitude Determination Algorithm Based on Antenna Configuration[J]. Journal of Electronics & Information Technology, 2017, 39(2): 459-465. doi: 10.11999/JEIT160347

Citation:

CUI Jianhua, CHENG Naiping. Attitude Determination Algorithm Based on Antenna Configuration[J]. Journal of Electronics & Information Technology, 2017, 39(2): 459-465. doi: 10.11999/JEIT160347

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Attitude Determination Algorithm Based on Antenna Configuration

doi: 10.11999/JEIT160347

CUI Jianhua^{1
,
,},
CHENG Naiping²

1.
2.
(Academy of Equipment, Beijing 101416, China)

Received Date: 2016-04-11
Rev Recd Date: 2016-08-30
Publish Date: 2017-02-19

Abstract

Abstract

In order to solve the problem of high computational complexity of the ambiguity in attitude measurement, a new attitude measurement method based on antenna configuration is proposed. In a certain range of measurement error, the antenna array for attitude determination is properly configured, the integer ambiguity of double difference carrier phase is determined by the constraint information of antenna configuration. Short-baseline and middle-baseline are used for coarse and precise attitude measurement. This method for aerocraft attitude determination does not need to solve the ambiguity. It avoids the use of complex ambiguity search algorithm and improves the speed of attitude determination, it is suitable for fast attitude measurement of aerocraft.
- Navigation,
- Attitude determination,
- Integer ambiguity

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References(22)

References

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