Fuel-Optimal Guidance for End-to-End Human-Mars Entry, Powered-Descent, and Landing Mission. - Changhuang Wan; Gangshan Jing; Ran Dai; Jeremy R. Rea (IEEE Trans. Aerosp. Electron. Syst., 2022)

A Hybrid ADMM for Six-Degree-of-Freedom Entry Trajectory Optimization Based on Dual Quaternions. - Chaoying Pei; Changhuang Wan; Ran Dai; Jeremy R. Rea (IEEE Trans. Aerosp. Electron. Syst., 2023)