Study on landing control method based on incremental dynamic inverse

Accurate landing control and improving the safety and reliability of the landing process are difficult issues in the safe recovery of carrier based aircraft. A landing control system based on incremental dynamic inverse is proposed. The method of an angle of attack maintenance loop and a trajectory rate control loop based on incremental dynamic inversion is used,which can achieve decoupling of angle of attack and trajectory,as well as direct control of trajectory by direct lift. A differential tracker is introduced to estimate the track angular acceleration signal required in the incremental dynamic inverse control law. The landing control system is verified with simulation. The results show that the designed landing control system based on incremental dynamic inverse has excellent control accuracy,speed,and robustness. It can achieve accurate tracking of the trajectory under different sea conditions interference,and the landing points can meet the quality requirements for the distribution of carrier based aircraft landing points.

Institutions

Publication Details

Journal
SHILAP Revista de lepidopterología
Published
2024-12-01
DOI
https://doi.org/10.16615/j.cnki.1674-8190.2024.06.12
Primary Topic
Aerospace and Aviation Technology
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Study on landing control method based on incremental dynamic inverse

SHILAP Revista de lepidopterología
Aerospace and Aviation Technology
article

Study on landing control method based on incremental dynamic inverse

article en

Abstract

Accurate landing control and improving the safety and reliability of the landing process are difficult issues in the safe recovery of carrier based aircraft. A landing control system based on incremental dynamic inverse is proposed. The method of an angle of attack maintenance loop and a trajectory rate control loop based on incremental dynamic inversion is used,which can achieve decoupling of angle of attack and trajectory,as well as direct control of trajectory by direct lift. A differential tracker is introduced to estimate the track angular acceleration signal required in the incremental dynamic inverse control law. The landing control system is verified with simulation. The results show that the designed landing control system based on incremental dynamic inverse has excellent control accuracy,speed,and robustness. It can achieve accurate tracking of the trajectory under different sea conditions interference,and the landing points can meet the quality requirements for the distribution of carrier based aircraft landing points.

SHILAP Revista de lepidopterología
Northwestern Polytechnical University (CN), Dynamic Research (United States) (US), Institute of Flight (US)
Life below water
Openalex Percentile: Top 40%
Aerospace and Aviation Technology
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

Study on landing control method based on incremental dynamic inverse · SHILAP Revista de lepidopterología (2024) | TGRS Research Map | TGRS