Fast Online Trajectory Generation for Time Adjustable Flight Consensus-Reference-Cited by-同舟云学术

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Fast Online Trajectory Generation for Time Adjustable Flight Consensus

Published:2024-05 Issue:3 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jiang Xi¹,Wang Jia¹,Zhao Bin²,Xie Jingjie³

Affiliation:

1. The 20th Research Institute, China Electronics Technology Group Corporation, Shaanxi, Xi’an 710068, China.

2. Professor, Institute of Precision Guidance and Control, Northwestern Polytechnical Univ., Shaanxi, Xi’an 710072, China.

3. Dept. of Aeronautical and Aviation Engineering, The Hong Kong Polytechnic Univ., Hung Hom, Kowloon, Hong Kong (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5090

Reference27 articles.

1. Nonsingular Sliding-Mode Control for Field-of-View Constrained Impact Time Guidance

2. Nonsingular Sliding Mode Guidance for Impact Time Control

3. Modified Pure Proportional Navigation Guidance Law for Impact Time Control

4. Varying-Gain Proportional Navigation Guidance for Precise Impact Time Control

5. Impact-Time Vector Guidance

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