Guidance Law Design for Terminal Area Energy Management of Reusable Launch Vehicle by Energy‐to‐Range Ratio

W Jiang, Z Yang - Mathematical Problems in Engineering, 2014 - Wiley Online Library
A new guidance scheme that utilizes a trajectory planning algorithm by energy‐to‐range
ratio has been developed under the circumstance of surplus energy for the terminal area …

Prediction-Correction Guidance Algorithm for High Velocity Reentry Capsules

J Chen, A Wang, W Tan, Y He, W Qiang… - 2021 40th Chinese …, 2021 - ieeexplore.ieee.org
Spacecraft returning from lunar or interplanetary missions reenter the Earth's atmosphere
with velocities that can approach 11 km/s. The landing position accuracy on the Earth is …

Optimal and Robust Control of Atmospheric Reentry Trajectories

AMP Moreira - 2022 - search.proquest.com
A reentrada na atmosfera terrestre é uma das fases mais difíceis da missão de qualquer
nave espacial. Durante a reentrada, seguir uma trajectória óptima em termos de taxa …

[PDF][PDF] Nonlinear Optimal Control of Reentry Vehicles Based on Deriving the State and Control Depended Systematic Matrices in State Space Form

A Hoseinzadeh, A Adami, A Ebrahimi - Journal of Space Science and …, 2018 - jsstpub.com
The atmospheric reentry phase is one of the most important mission steps in space
missions, therefore, the guidance and control of reentry vehicles in this phase of mission is …

Controlo Ótimo de Trajetórias Explícitas de Reentrada Atmosférica

LD dos Afeitos - 2014 - search.proquest.com
Controlo Ótimo de Trajetórias Explícitas de Reentrada Atmosférica Page 1 UNIVERSIDADE
DA BEIRA INTERIOR Engenharia Controlo Ótimo de Trajetórias Explícitas de Reentrada …

[引用][C] Controlo ótimo de trajetórias explícitas de reentrada atmosférica

LD Afeitos - 2014

[引用][C] کنترل بهینة غیرخطی وسایل بازگشت‌پذیر بر پایه استخراج ماتریس‌های سیستمی وابسته به متغیرهای حالت و کنترل در فرم فضای حالت

حسین زاده, آدمی, ابراهیمی - علوم و فناوری فضایی, 2018‎ - انجمن هوافضای ایران-پژوهشگاه هوافضا