Autonomous ascent guidance with multiple terminal constraints for all-solid launch vehicles

Author:

Zhang Qian,Xu Zhi

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Orbital suborbital program (OSP) minotaur space launch vehicle: low cost space lift for small satellites using surplus minuteman motors;Schoneman,2000

2. Solid propulsion systems for epsilon launch vehicle;Tokudome,2012

3. Multi-constrained ascent guidance for solid propellant launch vehicles;Xu;Aerosp. Sci. Technol.,2018

4. An approach and landing guidance design for reusable launch vehicle based on adaptive predictor-corrector technique;Li;Aerosp. Sci. Technol.,2018

5. An overview on flight dynamics and control approaches for hypersonic vehicles;Xu;Sci. China Inf. Sci.,2015

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