1–9 von 9 Ergebnissen
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    Computational Cost Evaluation of the Flight Controller Using Multi-hierarchy Dynamic Inversion for Winged Rocket

    Matsukami, Takahiro / Yonemoto, Koichi / Fujikawa, Takahiro et al. | Springer Verlag | 2019

    Attitude Control Law Design of Experimental Winged Rocket Using Engine Gimbal Control

    Sugimachi, Tomonori / Yonemoto, Koichi / Fujikawa, Takahiro | Springer Verlag | 2019

    Re-entry and Gliding Guidance Trajectory Optimization of Suborbital Spaceplane Using Dynamically Distributed Genetic Algorithm

    Koshida, Yasuhiro / Murakami, Masaaki / Fujikawa, Takahiro et al. | Springer Verlag | 2022

    Attitude Control of a Spaceplane Based on Dynamic Inversion Theory with Quaternion Error Calculation

    Kitazono, Yuto / Yonemoto, Koichi / Fujikawa, Takahiro et al. | Springer Verlag | 2022

    Separation Characteristics of a Two-Stage-To-Orbit Winged Rocket by Aerodynamic Interaction Analysis

    Otsuki, Tsuyoshi / Fujikawa, Takahiro / Yonemoto, Koichi | Springer Verlag | 2022

    Design and Development Status of Experimental Winged Rocket WIRES#015

    Watanabe, Akira / Yonemoto, Koichi / Fujikawa, Takahiro et al. | Springer Verlag | 2022

    Multi-objective System Optimization of Suborbital Spaceplane by Multi-fidelity Aerodynamic Analysis

    Tejika, Shintaro / Fujikawa, Takahiro / Yonemoto, Koichi | Springer Verlag | 2022

    Multiobjective Optimization of a Highly Maneuverable Supersonic Airfoil Using Multifidelity EGO

    Watanabe, Tomotaka / Yonemoto, Koichi / Fujikawa, Takahiro et al. | Springer Verlag | 2022