Lorenz et al., 2011 - Google Patents
A decoupled approach for trajectory generation for an unmanned rotorcraftLorenz et al., 2011
View PDF- Document ID
- 5365016709078415116
- Author
- Lorenz S
- Adolf F
- Publication year
- Publication venue
- Advances in Aerospace Guidance, Navigation and Control: Selected Papers of the 1st CEAS Specialist Conference on Guidance, Navigation and Control
External Links
Snippet
A decoupled approach to trajectory generation based on a cubic spline geometry formulation is introduced. The distinct consideration of boundary conditions yields a continuously differentiable trajectory definition such that path tracking errors are minimized …
- 239000000203 mixture 0 abstract description 6
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
- G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/04—Control of altitude or depth
- G05D1/042—Control of altitude or depth specially adapted for aircraft
- G05D1/046—Control of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/02—Control of position or course in two dimensions
- G05D1/021—Control of position or course in two dimensions specially adapted to land vehicles
- G05D1/0287—Control of position or course in two dimensions specially adapted to land vehicles involving a plurality of land vehicles, e.g. fleet or convoy travelling
- G05D1/0291—Fleet control
- G05D1/0295—Fleet control by at least one leading vehicle of the fleet
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/12—Target-seeking control
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0011—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement
- G05D1/0044—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot associated with a remote control arrangement by providing the operator with a computer generated representation of the environment of the vehicle, e.g. virtual reality, maps
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0005—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with arrangements to save energy
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106773713B (en) | High-precision nonlinear path tracking control method for under-actuated marine vehicle | |
Lu | Entry guidance: a unified method | |
Cho et al. | Three-dimensional nonlinear differential geometric path-following guidance law | |
Wang et al. | Line-of-sight guidance law for path following of amphibious hovercrafts with big and time-varying sideslip compensation | |
Mathisen et al. | Precision deep-stall landing of fixed-wing UAVs using nonlinear model predictive control | |
Schopferer et al. | Performance-aware flight path planning for unmanned aircraft in uniform wind fields | |
Fowler et al. | Bézier curve path planning for parafoil terminal guidance | |
Wang et al. | A fixed-wing UAV formation algorithm based on vector field guidance | |
Han et al. | Three-dimensional approach angle guidance under varying velocity and field-of-view limit without using line-of-sight rate | |
Stephan et al. | Precise tracking of extended three-dimensional dubins paths for fixed-wing aircraft | |
Lorenz et al. | A decoupled approach for trajectory generation for an unmanned rotorcraft | |
Garcia et al. | Robust geometric navigation of a quadrotor UAV on SE (3) | |
Galffy et al. | Nonlinear 3D path following control of a fixed-wing aircraft based on acceleration control | |
Seo et al. | Collision-avoided tracking control of UAV using velocity-adaptive 3D local path planning | |
Kawaguchi et al. | Stochastic approach to robust flight control design using hierarchy-structured dynamic inversion | |
Luo et al. | A guidance law for UAV autonomous aerial refueling based on the iterative computation method | |
Kim et al. | Robust path following control via command-filtered backstepping scheme | |
Sedlmair et al. | Design and experimental validation of UAV control laws-3D spline-path-following and easy-handling remote control | |
Chen et al. | Steady Glide Dynamics and Guidance of Hypersonic Vehicle | |
de la Cruz et al. | A streamlined nonlinear path following kinematic controller | |
Safwat et al. | Robust path following controller for unmanned aerial vehicle based on carrot chasing guidance law using dynamic inversion | |
Sedlmair et al. | Experimental comparison of nonlinear guidance laws for unmanned aircraft | |
Cho et al. | Three-dimensional nonlinear path-following guidance law based on differential geometry | |
Kim et al. | Evaluation of cooperative guidance for formation flight of fixed-wing UAVs using mesh network | |
Dugar et al. | Smooth trajectory optimization in wind: First results on a full-scale helicopter |