| A composite framework for co-optimization of spacecraft trajectory and propulsion system V Arya, E Taheri, JL Junkins Acta Astronautica 178, 773-782, 2021 | 33 | 2021 |
| Costate mapping for indirect trajectory optimization E Taheri, V Arya, JL Junkins Astrodynamics 5, 359-371, 2021 | 28 | 2021 |
| Low-thrust gravity-assist trajectory design using optimal multimode propulsion models V Arya, E Taheri, JL Junkins Journal of Guidance, Control, and Dynamics 44 (7), 1280-1294, 2021 | 27 | 2021 |
| Electric thruster mode-pruning strategies for trajectory-propulsion co-optimization V Arya, E Taheri, J Junkins Aerospace Science and Technology 116, 106828, 2021 | 26 | 2021 |
| ACCELERATION-BASED INDIRECT METHOD FOR CONTINUOUS AND IMPULSIVE TRAJECTORY DESIGN E Taheri, V Arya, JL Junkins 2021 AAS Astrodynamics Specialist Conference, 2021 | 9 | 2021 |
| Generation of multiple-revolution many-impulse optimal spacecraft maneuvers V Arya, K Şaloğlu, E Taheri, JL Junkins Journal of Spacecraft and Rockets 60 (6), 1699-1711, 2023 | 7 | 2023 |
| Hyperbolic tangent-based smoothing with state transition matrix implementation for generating fuel-optimal trajectories V Arya, E Taheri, J Junkins 29th AAS/AIAA Space Flight Mechanics Meeting, 2019 | 6 | 2019 |
| Finite element analysis of an index finger flexion in an extravehicular activity glove V Varya, W Scholten, R Fernandes, B Dunbar, DJ Hartl 2018 AIAA Modeling and Simulation Technologies Conference, 1927, 2018 | 6 | 2018 |
| Spacecraft Payload Maximization Using Realistic Multi-Mode Models of Electric Propulsion Systems V Arya, E Taheri, J Junkins 2021 American Control Conference (ACC), 1706-1711, 2021 | 4 | 2021 |
| Gravity-assist fuel-optimal low-thrust trajectory design using hybrid optimization techniques V Arya, E Taheri, R Woollands, JL Junkins Proceedings of the International Astronautical Congress, IAC 2019, IAC …, 2019 | 4 | 2019 |
| Indirect based shadow modelling with warm-up time for perturbed orbit transfers V Arya, R Woollands, JL Junkins Proceedings of the 44th Annual American Astronautical Society Guidance …, 2024 | 3 | 2024 |
| DESIGN OF LQR WEIGHTING MATRICES FOR TIME VARYING OUTPUT COVARIANCE ASSIGNMENT V Arya, R Goyal, M Majji, JL Junkins | 2 | 2021 |
| Connecting the Equinoctial Elements and Rodrigues Parameters: A New Set of Elements JTA Peterson, V Arya, JL Junkins Journal of Guidance, Control, and Dynamics 46 (9), 1726-1744, 2023 | 1 | 2023 |
| Nonlinearity Index for State-Costate Dynamics of Optimal Control Problems P Kelly, V Arya, JL Junkins, M Manoranjan | 1 | 2022 |
| A Composite Framework for Joint Optimization of Trajectory and Propulsion System Design V Arya, E Taheri, J Junkins AAS Guidance, Navigation and Control Conference, 20-015, 2020 | 1 | 2020 |
| Non-linear trajectory control of tensegrity prosthetic (protense) leg FNU Vishala | 1 | 2018 |
| INDIRECT BASED SHADOW MODELLING WITH WARM-UP TIME FOR PERTURBED ORBIT V Arya, R Woollands, JL Junkins Proceedings of the 44th Annual American Astronautical Society Guidance …, 2024 | | 2024 |
| Modelling of Low Frequency Variations in GRACE-FO Accelerometer Data using Onboard Thermal Data V Arya, A Peidou, N Harvey, FW Landerer AGU23, 2023 | | 2023 |
| Linear Quadratic Regulator Weighting Matrices for Output Covariance Assignment in Nonlinear Systems V Arya, R Goyal, M Majji, JL Junkins Journal of Guidance, Control, and Dynamics 46 (2), 264-276, 2023 | | 2023 |
| Novel Tools for Practical Co-optimization and Guidance of Space Missions FNU Vishala Texas A & M, 2022 | | 2022 |
Ehsan TaheriAssistant Professor, Auburn University在 auburn.edu 的电子邮件经过验证
Ehsan TaheriAssistant Professor, Auburn University在 auburn.edu 的电子邮件经过验证
Robyn WoollandsUniversity of Illinois / Jet Propulsion Lab在 illinois.edu 的电子邮件经过验证
Raman GoyalPalo Alto Research Center (PARC), SRI International在 sri.com 的电子邮件经过验证