Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control-Reference-Cited by-同舟云学术

Lunar Ascent and Orbit Injection via Neighboring Optimal Guidance and Constrained Attitude Control

Published:2018-09 Issue:5 Volume:31 Page:04018071
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Pontani Mauro¹^ORCID,Celani Fabio²

Affiliation:

1. Assistant Professor, Dept. of Astronautical, Electrical, and Energy Engineering, Sapienza Univ. of Rome, via Salaria 851, 00138 Rome, Italy (corresponding author). ORCID: .

2. Assistant Professor, School of Aerospace Engineering, Sapienza Univ. of Rome, via Salaria 851, 00138 Rome, Italy.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000908

Reference37 articles.

1. Determination of Nonlinear Optimal Feedback Law for Satellite Injection Problem Using Neighboring Optimal Control

2. Survey of Numerical Methods for Trajectory Optimization

3. Global and robust attitude control of a launch vehicle in exoatmospheric flight

4. Neighboring optimal trajectories for aeroassisted orbital transfer under uncertainties

5. A Survey of Methods Available for the Numerical Optimization of Continuous Dynamic Systems

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