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Stabilität
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Hybrid Intelligent Flight Control with Adaptive Learning Parameter Estimation
Comment on “Partial Integrated Missile Guidance and Control with Finite Time Convergence”
Methodology to Analyze Attitude Stability of Satellites Subjected to Aerodynamic Torques
Disturbance Rejection for an Unmanned Rotary Aircraft System Using Strain Sensing
Deviated Pursuit Based Interception at A Priori Fixed Time
Uniform Exponential Stability Result for the Rigid-Body Attitude Tracking Control Problem
Multiple-Timescale Nonlinear Control of Aircraft with Model Uncertainties
Trajectory Optimization for Multitarget Tracking Using Joint Probabilistic Data Association Filter
Identification of Linear Time-Periodic Systems from Rotorcraft Flight-Test Data
Modeling and Stability Analysis of Aerially Towed Systems Using Geometric Computational Dynamics
Control of an End Body Towed by a Circling Unmanned Aerial Vehicle
Three-Dimensional Nonlinear Cooperative Salvo Using Event-Triggered Strategy
Robust Tuning of Geometric Attitude Controllers for Multirotor Unmanned Aerial Vehicles
Data-Driven Method for Impact Time Control Based on Proportional Navigation Guidance
Identification of a Full-Envelope Learjet-25 Simulation Model Using a Stitching Architecture
Aircraft System Identification from Multisine Inputs and Frequency Responses
Frequency-Domain Bifurcation Analysis of a Nonlinear Flight Dynamics Model
Structured -Synthesis of Robust Attitude Control Laws for Quad-Tilt-Wing Unmanned Aerial Vehicle
Relaxed-Constraint Pinpoint Lunar Landing Using Geometric Mechanics and Model Predictive Control