He Linshu

Small launch vehicle trajectory profile optimization using hybrid algorithm

F. M. Villanueva, He Linshu, A. F. Rafique, 2013, Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST).

Nearly-orthogonal sampling and neural network metamodel driven conceptual design of multistage space launch vehicle

Mateen-ud-Din Qazi, He Linshu, Mateen-ud-Din Qazi, 2006, Comput. Aided Des..

Research on the method of target reconstruction guidance

He Linshu, Huang Yuqiu, 2011, 2011 Chinese Control and Decision Conference (CCDC).

Small Solid Propellant Launch Vehicle Mixed Design Optimization Approach

Xu Dajun, Fredy M. Villanueva, He Linshu, 2014 .

Support Vector Machine Based Trajectory Metamodel for Conceptual Design of Multi-stage Space Launch Vehicle

Saqlain Akhtar, He Linshu, 2005, CIS.

Multidisciplinary Design Optimization of Solid Launch Vehicle Using Hybrid Algorithm

Naeem Zafar, He Linshu, 2010 .

Kick Solid Rocket Motor Multidisciplinary Design Optimization Using Genetic Algorithm

Xu Dajun, Fredy M. Villanueva, He Linshu, 2013 .

Multi-Objective Hybrid Optimization for Multidisciplinary Conceptual Design of Solid Ballistic Missile

He Linshu, Naeem Zafar, 2009 .

Simulation-Based Optimization Strategy for Liquid Fueled Multi-stage Space Launch Vehicle

Saqlain Akhtar, He Linshu, 2005, Sixth International Conference on Parallel and Distributed Computing Applications and Technologies (PDCAT'05).

Optimal Trajectory Study of a Small Size Waverider and Wing-Body Reentry Vehicle at Suborbital Entry Speed of Approximately 4 km/s with Dynamic Pressure and Heat Rate Constraint

Tawfiqur Rahman, S. Tauqeer ul Islam Rizvi, He Linshu, 2012 .