Journals

[J11] Salahudden, S., Agrawal, A., Aditya Karnam, A., and Roy, A., " Decoupled Incremental Nonlinear Dynamic Inversion Control for Aircraft Autonomous Landing with Ground-Effect   Aerospace Science and Technology. https://doi.org/10.1016/j.ast.2024.109156

[J10] Salahudden, S., "Impact of Wind and Wind Shear on Aircraft Spin Recovery." Control Engineering Practice.https://doi.org/10.1016/j.conengprac.2024.105872

[J9] Dwivedi, V. S., Salahudden, S., Ghosh, A. K., and Kamath, G. M., Giri, D. K., “Achieving Zero Sideslip Angle Using Novel Surface Auxiron.” Journal of Guidance, Control and Dynamics. https://doi.org/10.2514/1.G006895.

[J8] Salahudden, S., and Joshi, H. V., “Aircraft Trajectory Generation and Control for Minimum Fuel and Time Efficient Climb.” Part G: Journal of Aerospace Engineering.https://doi.org/10.1177/09544100221126567 . 

[J7] Salahudden, S., and Ghosh, A. K., “Vertical Thrust Based Effective Flat-Spin Recovery of Aircraft Restricting Altitude Loss.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. https://doi.org/10.1177%2F09544100221089055

[J6] Salahudden, S., Das. A.T., and Ghosh, A. K., “Sliding-Mode Control and Strategic Thrust-Vectoring Based Aircraft Flat-Spin Recovery with Altitude Loss Minimization."  IEEE Transactions on Aerospace and Electronic Systems, Vol. 58, No. 4, pp. 3271-3282   https://doi.org/10.1109/TAES.2022.3146114.

[J5] Salahudden, S., Das, A. T., Jitu, S., Giri, D. K., and Ghosh, A. K., “Sliding-Mode Controller Based Aircraft Automatic Landing for Alternate Profiles.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. https://doi.org/10.1177%2F09544100211068903

[J4] Sanwale, J., Salahudden, S., Giri, D. K., “Neuro-Adaptive Fault-Tolerant Sliding Mode Controller for Spacecraft Attitude Stabilization .” AIAA Journal of Spacecraft and Rockets, Vol. 58, No. 6, 2021, pp. 1924–1929. https://doi.org/10.2514/1.A35058.

[J3] Salahudden, S., and Ghosh, A. K., “Robust Control Design Based Aircraft Flat-Spin Recovery Using Optimally Deflected Novel Deployable Fin.” Aerospace Science and Technology, Vol. 115, 2021, p. 106823. https://doi.org/10.1016/j.ast.2021.106823.

[J2] Salahudden, S., Dwivedi, V. S., Dwivedi, P. N., Giri, D. K., and Ghosh, A. K., “Aircraft Flat-Spin Recovery Using Sliding-Mode Based Attitude and Altitude Control.” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 235, No. 8, 2021, pp. 924–936. https://doi.org/10.1177/0954410020964674.

[J1] Dwivedi, V. S., Salahudden, S., Giri, D. K., Ghosh, A. K., and Kamath, G. M., “Optimal Energy Utilization for a Solar-Powered Aircraft Using Sliding-Mode-Based Attitude Control.” IEEE Transactions on Aerospace and Electronic Systems, Vol. 57, No. 1, 2021, pp. 105–118. https://doi.org/10.1109/TAES.2020.3015310.