位置：成果数据库 > 会议 > 会议详情页
Adaptive Height and Attitude Control of Small-scale Unmanned helicopter
  • 所属机构名称：中国人民解放军国防科学技术大学
  • 会议名称：2013 Chinese Conference of Decision and Control (CCDC2013)
  • 时间：2013.5.25
  • 成果类型：会议
  • 相关项目：混合过驱动系统容错控制分配研究
同会议论文项目
混合过驱动系统容错控制分配研究
期刊论文 8 会议论文 23
同项目会议论文
Adaptive Fault Diagnosis for Actuator Systems Based onObserver Parameters Estimation Algorithm
Generalized Two-stage Impact Angle Control Guidance Lawagainst Nonmaneuvering Targets
Adaptive Neural Dynamic Surface Attitude Control of a Quadrotor
Adaptive Non-homogeneous Higher Order Sliding Mode ControlWithout Switching Gain Overestimation
Adaptive Finite-time Attitude Tracking Control of an UncertainSpacecraft with Input Saturation
Real-Time Simulation for Online Identification of AircraftParameters Using Fourier Transform Regress
Fuzzy Control of Small-scale Unmanned helicopter
Adaptive Finite-time Tracking Control for a Robotic Manipulator withUnknown Deadzone
Dynamic Inversion Control with Guaranteed Transient andSteady State Performances for UAV systems
Adaptive Integrated Guidance and Control Design for a Missile With Input Constraints
Adaptive neural network control for aircraft landing under actuator failures
Fast nonsingular integral terminal sliding mode control for nonlinear dynamical systems
Non-homogeneous disturbance observer-based second order sliding mode control
Adaptive Neural Dynamic Surface Control for a Missile with Input and Output Constraints
SDRE Guidance Law for Impact Angle Control against MovingTargets
Backstepping Control for Longitudinal Dynamicsof Hypersonic Flight Vehicle
Design of The Optimal Glide Scheme for TheAirdropped Mine Using GPOPS
Intercepting Maneuvering Target with Specified Terminal Engagement GeometryUsing Variable Structure
Disturbance-observer-based second order sliding mode fault tolerant control for airbreathing hyperso
Non-homogeneous disturbance observer-based second order sliding mode control for a tailless aircraft
Robust adaptive sliding mode control for uncertain nonlinear MIMO system with guaranteed error bound
System identification of heave-yaw dynamics for small-scale unmanned helicopter using genetic algori