Six-Dimensional Atmosphere Entry Guidance based on Dual Quaternion
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Ran Dai | Chaoying Pei | Gangshan Jing | Changhuang Wan | Jeremy R. Rea | R. Dai | Changhuang Wan | Chaoying Pei | J. Rea | Gangshan Jing
[1] Ran Dai,et al. Alternating Minimization Algorithm for Polynomial Optimal Control Problems , 2019, Journal of Guidance, Control, and Dynamics.
[2] David B. Doman,et al. Optimal Trajectory Reconfiguration and Retargeting for Reusable Launch Vehicles , 2005 .
[3] I. Michael Ross,et al. Rapid Verification Method for the Trajectory Optimization of Reentry Vehicles , 2003 .
[4] Ping Lu,et al. Entry Guidance: A Unified Method , 2014 .
[5] P. Lu,et al. Optimal Aerocapture Guidance , 2015 .
[6] John Valasek,et al. Structured Adaptive Model Inversion Controller for Mars Atmospheric Flight , 2007 .
[7] John Valasek,et al. Fault‐tolerant control allocation for Mars entry vehicle using adaptive control , 2011 .
[8] Kevin P. Bollino. High-fidelity real-time trajectory optimization for reusable launch vehicles , 2006 .
[9] A. T. Yang,et al. Application of Dual-Number Quaternion Algebra to the Analysis of Spatial Mechanisms , 1964 .
[10] Ping Lu. Entry Guidance and Trajectory Control for Reusable Launch Vehicle , 1997 .
[11] Ping Lu. A year to remember. , 2016, Archives of disease in childhood.
[12] Mehran Mesbahi,et al. Constrained Autonomous Precision Landing via Dual Quaternions and Model Predictive Control , 2017 .