State-Space Perturbation Analytical Solution for the Dynamics of Launch-Vehicle Boost Phase-Reference-Cited by-同舟云学术

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State-Space Perturbation Analytical Solution for the Dynamics of Launch-Vehicle Boost Phase

Published:2024-09 Issue:5 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Deng Zexiao¹^ORCID,Liu Luhua²

Affiliation:

1. Ph.D. Candidate, School of Aeronautics and Astronautics, Shenzhen Campus of Sun Yat-sen Univ., Shenzhen, Guangdong 518107, China. ORCID:

2. Professor, School of Aeronautics and Astronautics, Shenzhen Campus of Sun Yat-sen Univ., Shenzhen, Guangdong 518107, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5523

Reference31 articles.

1. On the Integration of Linear Differential Equations

2. Error propagation properties for ICBM;Chen G.;J. Astronaut.,1984

3. Clark S. 2021. “Pegasus rocket successful in responsive launch demonstration.” Accessed June 13 2021. https://spaceflightnow.com/2021/06/13/pegasus-rocket-successful-in-responsive-launch-demonstration/.

4. Universal Gravity Turn Trajectories

5. Equations for Approximate Solutions Using Variational Calculus

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