Lyapunov-based guidance law for impact time control and simultaneous arrival
INTERCEPTOR guidance laws are designed to satisfy the primary requirement of driving to
zero the closing distance to the target. However, many practical engagements impose …
zero the closing distance to the target. However, many practical engagements impose …
[PDF][PDF] Multiple UAVs nonlinear guidance laws for stationary target observation with waypoint incidence angle constraint
Nonlinear guidance law combined with a pseudo pursuit guidance is proposed, to perform
stationary target observation mission. Multiple UAVs are considered, with waypoint …
stationary target observation mission. Multiple UAVs are considered, with waypoint …
[HTML][HTML] 基于空间两点的视觉自主着陆导引算法设计
魏祥灰， 唐超颖， 王彪 - 2019 - html.rhhz.net
为提高无人机着陆效率, 从着陆速度向量场和导引律设计两方面研究改进. 首先,
基于椭圆设计速度向量场, 实现飞行路程更短, 机动性能要求更低的着陆轨迹. 然后 …
基于椭圆设计速度向量场, 实现飞行路程更短, 机动性能要求更低的着陆轨迹. 然后 …
Development of an unmanned autonomous flying wing for aerial observations
T Fukuda, T Takimoto - 2014 14th International Conference on …, 2014 - ieeexplore.ieee.org
The unmanned aerial vehicles (UAVs) are the aircraft without a human operator on board.
Since operators can control the aircraft without some danger, they are useful as an …
Since operators can control the aircraft without some danger, they are useful as an …
Lyapunov-based missile terminal guidance with short time convergence considering seeker's first-order lag
D Zheng, D Lin, X Xu, Z Cheng - Proceedings of the …, 2017 - journals.sagepub.com
This paper presents a novel guidance law considering the seeker dynamics for
manoeuvring targets to achieve short homing time guidance using the Lyapunov method …
manoeuvring targets to achieve short homing time guidance using the Lyapunov method …
Turning direction determination using error dynamics-based guidance law for stationary target observation
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 …
stationary target observation missions. In this paper, a nonlinear guidance law is designed …
Visual guidance algorithm design for autonomous landing based on two points in space
X WEI, C TANG, B WANG - 北京航空航天大学学报, 2019 - bhxb.buaa.edu.cn
In order to increase the landing efficiency, improvements are made in two aspects: landing
velocity vector field and guidance law design. Landing velocity vector field is designed …
velocity vector field and guidance law design. Landing velocity vector field is designed …
궤환선형화기법을이용한무인항공기2 차원지상이동목표물추적유도기법
조남훈， 김유단 - 한국항공우주학회학술발표회초록집, 2013 - dbpia.co.kr
본 논문에서는 고정익 무인항공기가 지상에서 저속으로 이동하는 목표물을 거리를 두고
추적하기 위한 2 차원 비선형 유도기법을 제안하였다. 무인항공기와 목표물의 운동을 2 차원 …
추적하기 위한 2 차원 비선형 유도기법을 제안하였다. 무인항공기와 목표물의 운동을 2 차원 …
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 …
비선형 유도법칙을 다룬다. 시선각과 요구 충돌각의 오차로 정의된 시선각 오차 동역학을 …