Constrained predictor-corrector entry guidance
S Xue, P Lu - Journal of guidance, control, and dynamics, 2010 - arc.aiaa.org
WITH the advance in onboard computational capability, the class of predictor–corrector entry
guidance algorithms have received increasing attention. Applications considered over the …
guidance algorithms have received increasing attention. Applications considered over the …
Predictor-corrector entry guidance for low-lifting vehicles
P Lu - Journal of Guidance, Control, and Dynamics, 2008 - arc.aiaa.org
PREDICTOR-CORRECTOR entry guidance algorithms have long been used in mission
analyses and simulations for feasibility and trade studies of various entry vehicles and …
analyses and simulations for feasibility and trade studies of various entry vehicles and …
Skip entry trajectory planning and guidance
CW Brunner, P Lu - Journal of Guidance, Control, and Dynamics, 2008 - arc.aiaa.org
A numerical predictor–corrector method for trajectory planning and closed-loop guidance of
low-L= D vehicles during the skip entry phase of a lunar-return mission is presented. The …
low-L= D vehicles during the skip entry phase of a lunar-return mission is presented. The …
Gliding guidance of high L/D hypersonic vehicles
P Lu, S Forbes, M Baldwin - AIAA Guidance, Navigation, and Control …, 2013 - arc.aiaa.org
This paper investigates gliding guidance of hypersonic vehicles with high lift-to-drag (L/D)
ratios. The application scenarios envisioned are largely those that may be called suborbital …
ratios. The application scenarios envisioned are largely those that may be called suborbital …
[图书][B] Rapid simultaneous hypersonic aerodynamic and trajectory optimization for conceptual design
MJ Grant - 2012 - search.proquest.com
Simultaneously accounting for all major disciplines during the design of hypersonic vehicles
is challenging due to the computational requirements of high fidelity codes. As a result, a …
is challenging due to the computational requirements of high fidelity codes. As a result, a …
[图书][B] Introduction to astrodynamic reentry
KD Hicks - 2009 - apps.dtic.mil
This TR is actually a textbook on atmospheric entry for several classes at AFIT. It teaches
from an analytical perspective, with finding closed-form solutions being the preferred …
from an analytical perspective, with finding closed-form solutions being the preferred …
Crew exploration vehicle (CEV) skip entry trajectory
E Kaya - 2008 - scholar.afit.edu
This research effort develops a program using MATLAB® to solve the equations of motion
for the atmospheric reentry of the Crew Exploration Vehicle (CEV) which is assumed to be in …
for the atmospheric reentry of the Crew Exploration Vehicle (CEV) which is assumed to be in …
A Study on the Method of Spacecraft Deorbit Return Orbit Optimization
J Wenjuan, W Yajie, W Bin, C Xiao, Z Yan - International Conference On …, 2023 - Springer
The return trajectory optimization of spacecraft is a typical problem on optimal control. The
spacecraft is affected by quality, kinetic energy, aerodynamics, thermal flux, overload and so …
spacecraft is affected by quality, kinetic energy, aerodynamics, thermal flux, overload and so …
An improved predictor–corrector entry guidance method for hypersonic flight vehicle
W Fu, D Liu, K Chen, B Yan - Advances in Mechanical …, 2017 - journals.sagepub.com
This article improves an enhanced predictor–corrector entry guidance method for
hypersonic flight vehicle. To compensate for the shortcoming that the enhanced predictor …
hypersonic flight vehicle. To compensate for the shortcoming that the enhanced predictor …
Constrained Predictor-Corrector Entry Guidance
P Lu, S Xue - AIAA Guidance, Navigation, and Control Conference, 2009 - arc.aiaa.org
In this paper we develop a numerical predictor-corrector entry guidance algorithm for
vehicles with medium to higher lifting capability. A major difference between the current …
vehicles with medium to higher lifting capability. A major difference between the current …