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跨速域乘波体组合变体机翼布局及其任务能力评估

马铁林 景彪 蒋崇文 乔南璇 付竟成 向锦武

航空学报2026,Vol.47Issue(1):103-122,20.
航空学报2026,Vol.47Issue(1):103-122,20.DOI:10.7527/S1000-6893.2025.32051

跨速域乘波体组合变体机翼布局及其任务能力评估

Configuration design and mission capability evaluation of a cross-speed-range waverider-integrated morphing wing

马铁林 1景彪 2蒋崇文 2乔南璇 2付竟成 3向锦武1

作者信息

  • 1. 北京航空航天大学 无人系统研究院,北京 100191
  • 2. 北京航空航天大学 航空科学与工程学院,北京 100191
  • 3. 北京航空航天大学 沈元学院,北京 100191
  • 折叠

摘要

Abstract

Cross-speed-range vehicles have shown significant application potential in rapid deployment,persistent re-connaissance,and high-speed delivery.However,their development faces core challenges:a single aerodynamic configuration is often insufficient to accommodate complex flight condition requirements,and large monolithic platforms are difficult to adapt for swarm-based deployment.This study proposes a morphing glide vehicle configuration with swarm deployment capability and balanced cross-speed-range performance.The design integrates a waverider body with rotating and telescopic wings.A comprehensive framework is established,encompassing design,optimization,and performance evaluation,forming a closed-loop development process from mission requirement definition to perfor-mance validation for cross-speed-range morphing glide vehicles.In the system-level assessment,a parameter evalua-tion method based on a multi-stage reentry flight corridor is proposed.For aerodynamic optimization,a cross-speed-range optimization method is developed for the waverider tail fairing,along with a two-stage global-local optimization strategy for morphing wing design.Based on the hp-adaptive Radau Pseudospectral Method(hp-RPM),reachable domain computation and mission capability evaluation are performed.A dive-climb deceleration strategy suitable for this layout is proposed,enabling the vehicle to overcome quasi-equilibrium glide constraints and fulfill deceleration re-quirements without modifying the configuration,thereby improving its payload capacity.

关键词

跨速域布局设计/宽速域气动优化/乘波体/变体机翼/飞行器任务能力评估

Key words

cross-speed-range configuration design/wide-speed-range aerodynamic optimization/waverider/mor-phing wing/aircraft mission capability assessment

分类

航空航天

引用本文复制引用

马铁林,景彪,蒋崇文,乔南璇,付竟成,向锦武..跨速域乘波体组合变体机翼布局及其任务能力评估[J].航空学报,2026,47(1):103-122,20.

基金项目

航空科学基金(2024Z006051002) (2024Z006051002)

中央高校基本科研业务费专项资金(501QYJC2024129001) Aeronautical Science Foundation of China(2024Z006051002) (501QYJC2024129001)

the Fundamental Research Funds for the Central Universities(501QYJC2024129001) (501QYJC2024129001)

航空学报

1000-6893

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