Guidance Gain Analysis via Oscillation Motion of Error Dynamics-Based Guidance Law for Stationary...

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[PDF][PDF] Multiple UAVs nonlinear guidance laws for stationary target observation with waypoint incidence angle constraint

M Kim, Y Kim - International Journal Aeronautical and Space Sciences, 2013 - oak.go.kr
Nonlinear guidance law combined with a pseudo pursuit guidance is proposed, to perform
stationary target observation mission. Multiple UAVs are considered, with waypoint …
被引用次数：39 相关文章 所有 9 个版本
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Turning direction determination using error dynamics-based guidance law for stationary target observation

M Kim, Y Kim - Transactions of the Japan Society for Aeronautical …, 2014 - jstage.jst.go.jp
Guidance laws are proposed to enable unmanned aerial vehicles (UAVs) to accomplish
stationary target observation missions. In this paper, a nonlinear guidance law is designed …
被引用次数：1 相关文章 所有 5 个版本

충돌각조건을고려한시선각오차동역학기반의비선형유도법칙

김민구， 김유단 - 한국항공우주학회학술발표회초록집, 2011 - dbpia.co.kr
본 논문은 충돌각 조건이 주어졌을 때, 정지 목표물 타격을 위한 시선각 오차 동역학 기반의
비선형 유도법칙을 다룬다. 시선각과 요구 충돌각의 오차로 정의된 시선각 오차 동역학을 …
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