Modeling and Simulation on Optimum Maneuver Control Surface Configuration of Aircraft in Low Altitude Penetration Mode

Authors

Huzi Wu, 1. AVIC the First Aircraft Institute, Xi'an 710089, China; ;
Wang Jin, 2. AVIC Xi'an Civil Aircraft LTD, Xi'an 710089, China;
Wantao Qi, 1. AVIC the First Aircraft Institute, Xi'an 710089, China; ;
Kaibao Jin, 1. AVIC the First Aircraft Institute, Xi'an 710089, China; ;

Abstract

Abstract: Optimum maneuver control surface can ensure the safety flight cability of aircraft in low altitude penetration mode, and it is of great siginifcance to establish the valid and effective numerical simulation model. The numerical differential equations with muti-constraints is adopted for the first time, to construct the simulaton model for the aircraft with small wing load and mutifunctional and combined CS in low altitude manuever, the schemes of different maneuver CS considering the obstacle, the limit of angle of bank, the graident of climb are built. The simulation results show that the model is effective for solving the valid CS confiuration, which provides the theory evidence for manueve mode designing and important the design ideas to the CS system equipment.

Recommended Citation

Wu, Huzi; Jin, Wang; Qi, Wantao; and Jin, Kaibao (2021) "Modeling and Simulation on Optimum Maneuver Control Surface Configuration of Aircraft in Low Altitude Penetration Mode," Journal of System Simulation: Vol. 33: Iss. 9, Article 19.
DOI: 10.16182/j.issn1004731x.joss.20-0381
Available at: https://dc-china-simulation.researchcommons.org/journal/vol33/iss9/19

First Page

2180

Revised Date

2020-07-29

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.20-0381

Last Page

2190

CLC

TP391.9

Recommended Citation

Wu Huzi, Wang Jin, Qi Wantao, Jin Kaibao. Modeling and Simulation on Optimum Maneuver Control Surface Configuration of Aircraft in Low Altitude Penetration Mode[J]. Journal of System Simulation, 2021, 33(9): 2180-2190.

DOI

10.16182/j.issn1004731x.joss.20-0381