Guidance command generation and nonlinear dynamic inversion control for reusable launch vehicles-Reference-Cited by-同舟云学术

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Guidance command generation and nonlinear dynamic inversion control for reusable launch vehicles

Published:2020-09 Issue: Volume:174 Page:334-346
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Acquatella B Paul,Briese Lâle Evrim,Schnepper Klaus

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference60 articles.

1. Longterm/strategic scenario for reusable booster stages;Sippel;Acta Astronaut.,2006

2. Promising roadmap alternatives for the Spaceliner;Sippel;Acta Astronaut.,2010

3. Investigations of future expendable launcher options;Sippel,2011

4. Analysis of the Ariane 62/64 and Vega-C Launcher Family, Tech. Rep. DLR-IB-RY-HB-2016-63;Dumont,2016

5. Evaluation of a future reusable ariane VTOL booster;Dumont,2017

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1. U-control – a universal platform for control system design with inversion/cancellation of nonlinearity, dynamic and coupling through model-based to model-free procedures;International Journal of Systems Science;2024-08-27

2. Pseudospectral-Based Rapid Trajectory Planning and Feedforward Linearization Guidance;Drones;2024-08-02

3. Responsive tolerant control: An approach to extend adaptability of launch vehicles;Progress in Aerospace Sciences;2024-08

4. Wide-Speed Vehicle Control Considering Flight-Propulsion Coupling Constraints;Journal of Aerospace Engineering;2023-11

5. Finite-Horizon Near-Optimal Approach and Landing Planning of Reusable Launch Vehicles;Journal of Guidance, Control, and Dynamics;2023-03

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