Changzhu Wei

Orcid: 0000-0001-9279-479X

According to our database1, Changzhu Wei authored at least 11 papers between 2013 and 2021.

Collaborative distances:
  • Dijkstra number2 of five.
  • Erdős number3 of four.

Timeline

Legend:

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PhD thesis 
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Links

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Bibliography

2021
A convex approach to trajectory optimization for boost back of vertical take-off/vertical landing reusable launch vehicles.
J. Frankl. Inst., 2021

2020
Impact-Time-Control Guidance Law for Hypersonic Missiles in Terminal Phase.
IEEE Access, 2020

Multi-Process Integrated Planning and Guidance for Return of Reusable Aircraft Under Time Constraint.
IEEE Access, 2020

SVR-ND Method for Online Aerodynamic Parameter Estimation.
IEEE Access, 2020

A Novel Recurrent Convolutional Neural Network-Based Estimation Method for Switching Guidance Law.
IEEE Access, 2020

2019
Optimal Control of Ascent Trajectory for Launch Vehicles: A Convex Approach.
IEEE Access, 2019

2018
Non-Recursive Fixed-Time Convergence Observer and Extended State Observer.
IEEE Access, 2018

2016
Adaptive generalized super-twisting algorithm based guidance law design.
Proceedings of the 14th International Workshop on Variable Structure Systems, 2016

2015
A symplectic optimisation method for rapid endo-atmospheric ascent trajectory planning.
Int. J. Model. Identif. Control., 2015

A measurement method of nonlinear strength for dynamical model of SRLV.
Int. J. Model. Identif. Control., 2015

2013
Adaptive control for missile formation keeping under leader information unavailability.
Proceedings of the 10th IEEE International Conference on Control and Automation, 2013


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