Remote-control system of stratospheric airship and control method thereof

Through the four-level remote control system and multi-mode design, the complexity and fault tolerance problems of the stratospheric airship remote control system are solved, and efficient and reliable airship control is achieved, adapting to complex environments and fault conditions.

CN106828860AActive Publication Date: 2017-06-13BEIJING TIANHENG CHANGYING TECH CO LTD
5 Cites 9 Cited by

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
BEIJING TIANHENG CHANGYING TECH CO LTD
Filing Date
2017-03-01
Publication Date
2017-06-13

AI Technical Summary

Technical Problem

Due to the complex flight environment and high energy demand, the existing stratospheric airship remote control system is prone to insufficient energy supply or system failure. Moreover, the traditional single centralized control method is inefficient and has poor fault tolerance, and cannot meet the complex airship control needs.

Method used

A four-level remote control system is designed, including the decision-making layer, planning layer, execution layer and perception layer. It uses intelligent decision-making module, multimedia information integration module and recording and playback module to realize dynamic switching of flight mode and motor drive control, providing Standard mode, combined posture adjustment mode and failure mode, real-time monitoring and data collection to improve control efficiency and fault tolerance.

Benefits of technology

The airship's environmental adaptability and fault tolerance are significantly improved, the long-term control effect is enhanced, the control device is simplified and the control efficiency and reliability are improved.

✦ Generated by Eureka AI based on patent content.
Patent Text Reader

Abstract

The invention relates to a remote-control system of a stratospheric airship and a control method thereof. The control system is divided to four levels: a decision-making level for executing the selection and switch of a remote-control flight mode according to the actual working state data, and sending a corresponding mode command; a planning level for dynamically planning and generating an airship motor drive command according to the mode command sent by the decision-making level; an executing level for realizing the drive control to an airship motor according to the motor drive command of the planning level; and a perceiving level for finishing the real-time monitoring and data collection of the airship working state, and providing the original data of the airship working state to the decision-making level. The four-level control system architecture design of the control system is capable of simplifying the control device, improving the control efficiency, and fundamentally solving the problems of the function, efficiency and reliability of the near space airship ground and airborne control system.
Need to check novelty before this filing date? Find Prior Art

Citation Information

Patent Citations

  • Low-altitude airship flight control system and flight control method thereof

    CN102033546A

  • Stratospheric-airship-analytic-model-based prediction path tracking control method

    CN105116914A

  • Guidance and control integration and control distribution method of stratospheric airship

    CN105173051A

  • Semi-independent flight control system of unmanned airship and control method thereof

    CN1557676A

  • Apparatus for distributed airborne wireless communications

    US8983455B1

Cited By

  • Control system and method for fixed-point parking of stratospheric aerostat

    CN110244754A

  • A control system and method for stationary hovering of a stratospheric airship

    CN110244754B

  • Unmanned airship avoidance system and unmanned airship flight control system

    CN110673638A

  • An unmanned airship obstacle avoidance system and an unmanned airship flight control system

    CN110673638B

  • Stratospheric airship energy supply state monitoring method for aid decision

    CN113178924A