Kim et al., 2006 - Google Patents
System identification and 6-DOF hovering controller design of unmanned model helicopterKim et al., 2006
View PDF- Document ID
- 6834124286327771577
- Author
- Kim B
- Chang Y
- Lee M
- Publication year
- Publication venue
- JSME International Journal Series C Mechanical Systems, Machine Elements and Manufacturing
External Links
Snippet
For a maneuvering unmanned autonomous helicopter, it is necessary to design a proper controller for each flight mode. In this paper, the overall helicopter dynamics is derived and a hovering model is linearized and transformed into a state-space form. However, since it is …
- 238000004088 simulation 0 abstract description 13
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
- G05D1/0011—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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
- G05D1/104—Simultaneous control of position or course in three dimensions specially adapted for aircraft involving a plurality of aircrafts, e.g. formation flying
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Sydney et al. | Dynamic control of autonomous quadrotor flight in an estimated wind field | |
Bouadi et al. | Adaptive sliding mode control for quadrotor attitude stabilization and altitude tracking | |
Kim et al. | System identification and 6-DOF hovering controller design of unmanned model helicopter | |
Bogdanov et al. | State-dependent Riccati equation control of a small unmanned helicopter | |
Soneson et al. | Simulation testing of advanced response types for ship-based rotorcraft | |
Choi et al. | System identification-based sliding mode control for small-scaled autonomous aerial vehicles with unknown aerodynamics derivatives | |
Ansari et al. | Development and experimental investigation of a Quadrotor’s robust generalized dynamic inversion control system | |
Niemiec et al. | Multirotor controls, trim, and autonomous flight dynamics of plus-and cross-quadcopters | |
He et al. | Acceleration-feedback-enhanced robust control of an unmanned helicopter | |
Kumar et al. | Differential flatness based hybrid PID/LQR flight controller for complex trajectory tracking in quadcopter UAVs | |
Trenev et al. | Movement stabilization of the parrot mambo quadcopter along a given trajectory based on PID controllers | |
Krishnamurthi et al. | Helicopter slung load control using lagged cable angle feedback | |
Bogdanov et al. | SDRE flight control for X-Cell and R-Max autonomous helicopters | |
Wei et al. | System identification of wind effects on multirotor aircraft | |
Lv et al. | A multivariate optimal control strategy for the attitude tracking of a parafoil-UAV system | |
González et al. | Loop-separation control for very flexible aircraft | |
Salinas et al. | Unified motion control for multilift unmanned rotorcraft systems in forward flight | |
Kim et al. | Design of 6-dof attitude controller of hovering model helicopter | |
Xu et al. | Modelling and hovering control of a novel multi-tandem ducted fan vehicle | |
Mukarram et al. | Altitude control of a quadcopter | |
Singh et al. | Slung load stabilization across the flight envelope using an active cargo hook | |
Mahfouz et al. | Quadrotor unmanned aerial vehicle controller design and synthesis | |
Haviland et al. | Rapid automatic slung load operations with unmanned helicopters | |
de Oliveira et al. | Dynamic modelling and control of unmanned aerial vehicle of the quadrotor type | |
Hachem et al. | Improving Incremental Nonlinear Dynamic Inversion Robustness Using Robust Control in Aerial Robotics |