Lecheng Liang
Orcid: 0000-0003-1500-9553
According to our database1,
Lecheng Liang authored at least 4 papers
between 2024 and 2026.
Collaborative distances:
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Bibliography
2026
Terminal Point Deviation-Involved Rapid Ascent Trajectory Planning for RBCC-Powered Aerospace Plane.
IEEE Trans. Aerosp. Electron. Syst., 2026
2025
Nonlinearity-Kept Picard-Newton's Method-Based Ascending Trajectory Planning for Single-Stage-to-Orbit Aerospace Plane With Combined-Cycle Propulsion.
IEEE Trans. Aerosp. Electron. Syst., December, 2025
2024
Combined-Cycle Propulsion-Involved Trajectory Optimization and Performance-Driven Attitude Control for Aerospace Plane During the Ascent Phase.
IEEE Trans. Intell. Transp. Syst., December, 2024
Impact angle controlled integrated guidance and control with input and state constraints.
Int. J. Control, April, 2024