Linear Optimal Guidance for an AIM-9L Missile

1981 ◽  
Vol 4 (5) ◽  
pp. 662-663 ◽  
Author(s):  
Paul L. Vergez
Keyword(s):  
Optimal Guidance

An Approach to Optimal Guidance of an Advanced Lauch Vehicle Concept

1990 ◽  
Author(s):  
Martin S. Leung ◽  
Anthony J. Calise
Keyword(s):  
Vehicle Concept ◽  
Optimal Guidance

Optimal Guidance LAM Implementation Issues

1988 ◽  
Author(s):  
J. H. Evers ◽  
J. R. Cloutier ◽  
F. Zupancic
Keyword(s):  
Optimal Guidance

A Practical Optimal Guidance Scheme Under Impact Angle and Terminal Acceleration Constraints

2021 ◽  
Author(s):  
Hyo-Seon Chi ◽  
Yong-In Lee ◽  
Chang-Hun Lee ◽  
Han-Lim Choi
Keyword(s):  
Impact Angle ◽  
Optimal Guidance

scholarly journals Neighboring Optimal Guidance and Constrained Attitude Control for Accurate Orbit Injection

2021 ◽  
Author(s):  
Mauro Pontani ◽  
Fabio Celani
Keyword(s):  
Attitude Control ◽  
Initial Position ◽  
Low Earth Orbit ◽  
Guidance And Control ◽  
Optimal Guidance ◽  
Combined Use ◽  
Upper Stage ◽  
Neighboring Optimal Guidance ◽  
And Control ◽  
Guidance Technique

AbstractAccurate orbit injection represents a crucial issue in several mission scenarios, e.g., for spacecraft orbiting the Earth or for payload release from the upper stage of an ascent vehicle. This work considers a new guidance and control architecture based on the combined use of (i) the variable-time-domain neighboring optimal guidance technique (VTD-NOG), and (ii) the constrained proportional-derivative (CPD) algorithm for attitude control. More specifically, VTD-NOG & CPD is applied to two distinct injection maneuvers: (a) Hohmann-like finite-thrust transfer from a low Earth orbit to a geostationary orbit, and (b) orbit injection of the upper stage of a launch vehicle. Nonnominal flight conditions are modeled by assuming errors on the initial position, velocity, attitude, and attitude rate, as well as actuation deviations. Extensive Monte Carlo campaigns prove effectiveness and accuracy of the guidance and control methodology at hand, in the presence of realistic deviations from nominal flight conditions.

Boost-glide range-optimal guidance

2007 ◽  
Vol 3 (3) ◽  
pp. 293-298 ◽  
Author(s):  
H. J. Kelley ◽  
E. M. Cliff ◽  
F. H. Lutze
Keyword(s):  
Optimal Guidance

A new neuro-based solution for closed-loop optimal guidance with terminal constraints

1999 ◽  
Author(s):  
N. Rahbar ◽  
M. Bahrami ◽  
M. Menhaj
Keyword(s):  
Closed Loop ◽  
Optimal Guidance ◽  
Terminal Constraints

scholarly journals A Computationally Inexpensive Optimal Guidance via Radial-Basis-Function Neural Network for Autonomous Soft Landing on Asteroids

PLoS ONE ◽  
2015 ◽  
Vol 10 (9) ◽  
pp. e0137792 ◽  
Author(s):  
Peng Zhang ◽  
Keping Liu ◽  
Bo Zhao ◽  
Yuanchun Li
Keyword(s):  
Neural Network ◽  
Radial Basis Function ◽  
Basis Function ◽  
Soft Landing ◽  
Optimal Guidance ◽  
Radial Basis

Stochastic Approach to Optimal Guidance with Uncertain Intercept Time

2010 ◽  
Vol 46 (4) ◽  
pp. 1804-1820 ◽  
Author(s):  
Gyorgy Hexner ◽  
Haim Weiss
Keyword(s):  
Stochastic Approach ◽  
Optimal Guidance
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