GPS Attitude Determination Algorithm and its Evaluation by Aircraft Flight Test
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概要
- 論文の詳細を見る
- 2001-03-01
著者
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NAKAJIMA Ken
Mitsubishi Materials Corp., Silicon Research Center
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Inagaki Toshiharu
National Aerospace Laboratory Of Japan Flight Systems Research Center
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Ishijima Yoshiyuki
National Space Development Agency Of Japan Guidance Control And Dynamics Group
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MIYANO Tomoyuki
National Space Development Agency of Japan Guidance, Control and Dynamics Group
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SUZUKI Hideto
National Space Development Agency of Japan Guidance, Control and Dynamics Group
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HARIGAE Masatoshi
National Aerospace Laboratory of Japan Flight Systems Research Center
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FUJIWARA Takeshi
National Aerospace Laboratory of Japan Flight Systems Research Center
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NAGANO Kotaro
Mitsubishi Space Software
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KOBORI Takehiko
Mitsubishi Space Software
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Suzuki Hideto
National Space Development Agency Of Japan Guidance Control And Dynamics Group
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Miyano Tomoyuki
National Space Development Agency Of Japan Guidance Control And Dynamics Group
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Nakajima Ken
Mitsubishi Materials Corp. Silicon Research Center
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Nakajima Ken
Mitsubishi Space Software
関連論文
- Measurement of Young's Modulus of Silicon Single Crystal at High Temperature and Its Dependency on Boron Concentration Using the Flexural Vibration Method
- GPS Attitude Determination Algorithm and its Evaluation by Aircraft Flight Test
- GPS-basde Space Navigation : Comparison of Antenna Configuration for Launch Vehicle
- Development of GPS Aided Inertial Navigation System for High Speed Flight Demonstrator