A. Shirazi

An evolutionary discretized Lambert approach for optimal long-range rendezvous considering impulse limit

Jose A. Lozano, Josu Ceberio, Abolfazl Shirazi, 2019, Aerospace Science and Technology.

Design and performance simulation of a satellite momentum exchange actuator

Mehran Mirshams, Abolfazl Shirazi, M. Mirshams, 2016 .

Spacecraft trajectory optimization: A review of models, objectives, approaches and solutions

Jose A. Lozano, Josu Ceberio, Abolfazl Shirazi, 2018, Progress in Aerospace Sciences.

EDA++: Estimation of Distribution Algorithms With Feasibility Conserving Mechanisms for Constrained Continuous Optimization

J. A. Lozano, Josu Ceberio, A. Shirazi, 2022, IEEE Transactions on Evolutionary Computation.

Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission

A. H. Mazinan, Abolfazl Shirazi, A. Shirazi, 2016 .

Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission

A. Mazinan, A. Shirazi, 2015, Computational and Applied Mathematics.

Trajectory optimization of space vehicle in rendezvous proximity operation with evolutionary feasibility conserving techniques

J. A. Lozano, Josu Ceberio, A. Shirazi, 2023, Eng. Appl. Artif. Intell..

Analysis of a hybrid genetic simulated annealing strategy applied in multi-objective optimization of orbital maneuvers

Abolfazl Shirazi, A. Shirazi, 2017, IEEE Aerospace and Electronic Systems Magazine.

Evolutionary algorithms to optimize low-thrust trajectory design in spacecraft orbital precession mission

José Antonio Lozano, Josu Ceberio, Abolfazl Shirazi, 2017, 2017 IEEE Congress on Evolutionary Computation (CEC).

Trajectory optimization of spacecraft high-thrust orbit transfer using a modified evolutionary algorithm

Abolfazl Shirazi, A. Shirazi, 2016 .