NAVIGATIOAN CONTROL SYSTEM OF UNMANNED AIRVEHICLE BASED ON TMO MODEL AND THE CONTROL METHOD OF THE SAME

NAVIGATIOAN CONTROL SYSTEM OF UNMANNED AIRVEHICLE BASED ON TMO MODEL AND THE CONTROL METHOD OF THE SAME

Disclosed are a navigation control system of an unmanned air vehicle based on a TMO model, and a control method thereof. According to embodiments of the present invention, a more stable and reliable system is able to be constructed since a plurality of TMO models are constructed and operated as an i...

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Bibliographische Detailangaben
Hauptverfasser: KIM, JUNG GUK, JUNG, EUN HAE, KIM, YONG HYUN, AHN, MI RIM
Format: Patent
Sprache:eng ; kor
Schlagworte:
CALCULATING
COMPUTING
COUNTING
ELECTRIC DIGITAL DATA PROCESSING
PHYSICS
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Beschreibung
Zusammenfassung:Disclosed are a navigation control system of an unmanned air vehicle based on a TMO model, and a control method thereof. According to embodiments of the present invention, a more stable and reliable system is able to be constructed since a plurality of TMO models are constructed and operated as an individual partition. In addition, by using control information calculated by the other TMO model for controlling an air vehicle if an error occurs in one TMO model, the present invention enables to control the unmanned air vehicle as well as being widely applied to a field requiring a real-time control. 티엠오(TMO) 모델 기반의 무인 비행체의 항법 제어 시스템 및 이의 제어방법에 개시된다. 본 발명의 실시예들에 의하면, 복수의 티엠오(TMO) 모델이 각각 독립적인 파티션으로 구축 및 동작하도록 구현함으로써, 보다 안정되고 신뢰성 있는 시스템을 구축할 수 있다. 또한, 하나의 티엠오(TMO) 모델에 오류가 발생한 경우에 또 다른 티엠오(TMO) 모델에 의해 산출된 제어정보를 비행체 제어에 사용함으로써, 무인 비행체 제어뿐만 아니라, 실시간 제어를 다른 요하는 분야에서도 넓게 적용될 수 있다.