A Control Method for Multi-Missile Cooperative Operation
A technology of multiple missiles and control methods, applied in the field of guidance
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0075] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0076] At present, in the field of multi-missile cooperative combat research, how to control each missile to simultaneously hit the target from different directions and specified angles in three-dimensional space is an important issue to improve the missile's defense penetration capability and enhance the missile's ability to strike the target . In the present invention:
[0077] As shown in Figure 1, first introduce the concept of virtual leader missiles, and assume that the virtual leader missiles fly vertically and laterally using the enhanced proportional guidance law; Set the angle to adjust the missile-to-target distance, so that the missile-to-target distance can track the missile-to-target distance of the virtual leader missile, so as to obtain the coordinated guidance law that can make multiple missiles attack the target at the same...
PUM
![No PUM](https://static-eureka.patsnap.com/ssr/23.2.0/_nuxt/noPUMSmall.5c5f49c7.png)
Abstract
Description
Claims
Application Information
![application no application](https://static-eureka.patsnap.com/ssr/23.2.0/_nuxt/application.06fe782c.png)
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com