How Mathematical Modelling and Optimisation Guide Spacecraft Trajectories
Spacecraft trajectory design is fundamentally a mathematical problem involving the prediction, evaluation and optimisation of motion under complex physical constraints.
Journal of Aerospace Engineering & Technology Journal of Aerospace Engineering & Technology (JOAET)Â is a peer-reviewed hybrid open-access journal launched in 2011, focused on the rapid publication of fundamental and multidisciplinary research papers on all areas of Aerospace Engineering …
joaet maintains an Editorial Board of practicing researchers from around the world, to ensure manuscripts are handled by editors who are experts in the field of study.

Institutional Profile Link: https://hindustanuniv.ac.in/assets/img/aero_dept/fac-pro/aero-shah-profile.pdf
Spacecraft trajectory design is fundamentally a mathematical problem involving the prediction, evaluation and optimisation of motion under complex physical constraints.
Leading-Edge Roughness (LER) strongly dictates boundary layer transition and performance degradation on an airfoil operating at transitional Reynolds numbers, an aerodynamic regime where shear-layer stability mechanisms remain highly complex.
A significant challenge for autonomous drone landings in unstructured environments is that of reliably detecting and identifying objects in real-time to ensure safety and accuracy of the landing area.
The rapid development of reusable hypersonic space transportation systems has intensified the need for advanced thermal protection technologies capable of withstanding extreme aerodynamic heating conditions encountered during atmospheric re-entry and sustained hypersonic flight.
Estimating the Remaining Useful Life (RUL) of industrial machinery in real-time is now vital for both operational safety and smart resource management.
Aerospike nozzles are gaining attention as a more advanced alternative to conventional bell nozzles, mainly because they can perform efficiently across a wide range of altitude conditions.