Near optimal guidance law for descent to a point using inverse problem approach
An explicit guidance law that maximizes terminal velocity is developed for a reentry vehicle
to a fixed target. Motion is constrained to an optimal, three-dimensional Bezier curve …
to a fixed target. Motion is constrained to an optimal, three-dimensional Bezier curve …
An Explicit Reentry Guidance Law Using Bezier Curves
R Esmaelzadeh, A Naghash… - Transactions of the Japan …, 2008 - jstage.jst.go.jp
An explicit guidance law is developed for a reentry vehicle. Motion is constrained to a three-
dimensional Bezier curve. Acceleration commands are derived by solving an inverse …
dimensional Bezier curve. Acceleration commands are derived by solving an inverse …
Review of Re-entry Guidance Methods Based on Trajectory Generation
R Esmaelzadeh, FZ Rahmani - Technology in Aerospace Engineering, 2022 - jtae.ari.ac.ir
One of the most important and complex issues in the field of aerospace engineering is the
returning to the atmosphere. Many flying objects do not experience returning to the …
returning to the atmosphere. Many flying objects do not experience returning to the …
Near optimal re-entry guidance law using inverse problem approach
R Esmaelzadeh, A Naghash… - Inverse Problems in …, 2008 - Taylor & Francis
An explicit guidance law that maximizes terminal velocity is developed for a re-entry vehicle
to a fixed target. Motion is constrained to an optimal, 3D Bezier curve. Acceleration …
to a fixed target. Motion is constrained to an optimal, 3D Bezier curve. Acceleration …
[PDF][PDF] یملع-یجیورت
RE Aval, FZ Rahmani - sid.ir
One of the most important and complex issues in the field of aerospace engineering is the
returning to the atmosphere. Many flying objects do not experience returning to the …
returning to the atmosphere. Many flying objects do not experience returning to the …
مروری بر روش‌های هدایت ورود به جو مبتنی بر تولید مسیر
اسماعیل‌زاده, رحمانی, فاطمه زهرا - فناوری در مهندسی هوافضا, 2022 - jtae.ari.ac.ir
یکی از مسائل مهم و پیچیده در حوزة مهندسی هوافضا، مسئلة بازگشت به جو است. در بسیاری از
وسائل پرنده پدیدة بازگشت به جو مورد بررسی قرار نمی‌گیرد، چراکه آن را تجربه نمی‌کنند. مطالعة …
وسائل پرنده پدیدة بازگشت به جو مورد بررسی قرار نمی‌گیرد، چراکه آن را تجربه نمی‌کنند. مطالعة …
[PDF][PDF] On-board near optimal flight trajectory generation using deferential flatness
R Esmaelzadeh - International Journal of Computer Applications, 2014 - Citeseer
An optimal explicit guidance law that maximizes terminal velocity is developed for a reentry
vehicle to a fixed target. The equations of motion are reduced with differential flatness …
vehicle to a fixed target. The equations of motion are reduced with differential flatness …
[PDF][PDF] Explicit Flatness-Based Guidance in Reentry Phase
R Esmaelzadeh - Space Science and Technology, 2014 - jsstpub.com
An explicit guidance law is developed for a reentry vehicle. Motion is constrained to a three-
dimensional Bezier curve. Acceleration commands are derived by solving an inverse …
dimensional Bezier curve. Acceleration commands are derived by solving an inverse …
Flatness-based Near Optimal Guidance
An optimal explicit guidance law that maximizes terminal velocity is developed for the
reentry of a vehicle to a fixed target. The equations of motion are reduced with differential …
reentry of a vehicle to a fixed target. The equations of motion are reduced with differential …
هدایت صریح نزدیک بهینه مبتنی بر همواری دیفرانسیلی
اسماعیل زاده رضا, نقاش ابوالقاسم, مرتضوی بک مهدی - 2017 - sid.ir
در این مقاله یک قانون هدایت بهینه مبتنی بر همواری دیفرانسیلی برای بیشینه سازی سرعت
نهایی وسایل پرنده توسعه داده می شود. معادلات حرکت با رویکرد همواری دیفرانسیلی کاهش می یابد …
نهایی وسایل پرنده توسعه داده می شود. معادلات حرکت با رویکرد همواری دیفرانسیلی کاهش می یابد …