Ehsan Taheri, Ph.D.
Affiliations: | 2014 | Mechanical Engineering-Engineering Mechanics | Michigan Technological University, USA |
Area:
Mechanical Engineering, Aerospace EngineeringGoogle:
"Ehsan Taheri"Parents
Sign in to add mentorOssama Abdelkhalik | grad student | 2014 | Michigan Technological University | |
(Rapid space trajectory generation using a Fourier series shape-based approach.) |
BETA: Related publications
See more...
Publications
You can help our author matching system! If you notice any publications incorrectly attributed to this author, please sign in and mark matches as correct or incorrect. |
Davoudi B, Taheri E, Duraisamy K, et al. (2020) Quad-Rotor Flight Simulation in Realistic Atmospheric Conditions Aiaa Journal. 58: 1992-2004 |
Mall K, Grant MJ, Taheri E. (2020) Uniform Trigonometrization Method for Optimal Control Problems with Control and State Constraints Journal of Spacecraft and Rockets. 1-13 |
Taheri E, Junkins JL, Kolmanovsky I, et al. (2020) A novel approach for optimal trajectory design with multiple operation modes of propulsion system, part 2 Acta Astronautica. 172: 166-179 |
Taheri E, Junkins JL, Kolmanovsky IV, et al. (2020) A novel approach for optimal trajectory design with multiple operation modes of propulsion system, part 1 Acta Astronautica. 172: 151-165 |
Singh SK, Woollands R, Taheri E, et al. (2020) Feasibility of quasi-frozen, near-polar and extremely low-altitude lunar orbits Acta Astronautica. 166: 450-468 |
Saghamanesh M, Taheri E, Baoyin H. (2020) Interplanetary gravity-assist fuel-optimal trajectory optimization with planetary and Solar radiation pressure perturbations Celestial Mechanics and Dynamical Astronomy. 132: 16 |
Junkins JL, Taheri E. (2019) Exploration of Alternative State Vector Choices for Low-Thrust Trajectory Optimization Journal of Guidance, Control, and Dynamics. 42: 47-64 |
Saghamanesh M, Taheri E, Baoyin H. (2019) Systematic low-thrust trajectory design to Mars based on a full Ephemeris modeling Advances in Space Research. 64: 2356-2378 |
Taheri E, Junkins JL. (2019) How Many Impulses Redux The Journal of the Astronautical Sciences. 67: 257-334 |
Woollands R, Taheri E, Junkins JL. (2019) Efficient Computation of Optimal Low Thrust Gravity Perturbed Orbit Transfers The Journal of the Astronautical Sciences. 67: 458-484 |