Geometry and time updaters-based arbitrary-yaw iterative explicit guidance for fixed-thrust boost back of vertical take-off/vertical landing reusable launch vehicles-Reference-Cited by-同舟云学术

Geometry and time updaters-based arbitrary-yaw iterative explicit guidance for fixed-thrust boost back of vertical take-off/vertical landing reusable launch vehicles

Published:2019-12 Issue: Volume:95 Page:105433
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wei Changzhu,Ju Xiaozhe,Wu Rong,He Yanfeng,Diao Yin

Funder

Harbin Science and Technology Innovation Talents Fund

Publisher

Elsevier BV

Subject

Aerospace Engineering

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5. Fixed-time trajectory tracking for a quadrotor with external disturbances: a flatness-based sliding mode control approach;Ai;Aerosp. Sci. Technol.,2019

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