Liu et al., 2017 - Google Patents
LQG based model predictive control for gust load alleviationLiu et al., 2017
View PDF- Document ID
- 4337520232483896578
- Author
- Liu X
- Sun Q
- Cooper J
- Publication year
- Publication venue
- Aerospace science and Technology
External Links
Snippet
A linear quadratic Gaussian (LQG) based model predictive control (MPC) method is proposed to alleviate the dynamic gust loads of flexible aircrafts flying through turbulence, utilizing look-ahead information of the turbulence via light detection and ranging (LIDAR) …
- 238000000034 method 0 abstract description 23
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
- G05D1/04—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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Liu et al. | LQG based model predictive control for gust load alleviation | |
| Tohidi et al. | Adaptive control allocation for constrained systems | |
| Ward et al. | Adaptive glide slope control for parafoil and payload aircraft | |
| Shen et al. | Micro air vehicle’s attitude control using real-time pressure and shear information | |
| Juang et al. | Disturbance encountered landing system design based on sliding mode control with evolutionary computation and cerebellar model articulation controller | |
| Mori et al. | Neural network modeling of lateral pilot landing control | |
| Zhen et al. | Modeling, control design, and influence analysis of catapult-assisted take-off process for carrier-based aircrafts | |
| Han et al. | Robust autopilot design for STT missiles with multiple disturbances using twisting control | |
| Rong et al. | Robust control for an unmanned helicopter with constrained flapping dynamics | |
| Deittert et al. | Dynamic soaring flight in turbulence | |
| Li et al. | Modeling landing signal officer instruction associated with operation guide system | |
| Venkataraman et al. | Reliability assessment of actuator architectures for unmanned aircraft | |
| Ehlers et al. | Wake impact alleviation control based on wake identification | |
| Ma et al. | Optimization design study of low-Reynolds-number high-lift airfoils for the high-efficiency propeller of low-dynamic vehicles in stratosphere | |
| Wu et al. | An approach to estimate aircraft touchdown attitudes and control inputs | |
| Haridas et al. | Longitudinal guidance of unmanned aerial vehicle using integral sliding mode control | |
| Pontillo | High aspect ratio wings on commercial aircraft: a numerical and experimental approach | |
| Hoencamp et al. | Concept of a predictive tool for ship–helicopter operational limitations of various in-service conditions | |
| Khan et al. | An adaptive flare scheme for autonomous landing of a fixed-wing UAV | |
| Wang et al. | Design of automatic carrier-landing controller based on compensating states and dynamic inversion | |
| Bukov et al. | A predictive algorithm for runway overrun protection | |
| Gonzalez et al. | Design of a landing control system which considers dynamic ground effect for an unmanned airplane | |
| Karimtaevna et al. | Robust control of aircraft flight in conditions of disturbances | |
| Chen et al. | Design of a controller for morphing aircraft based on backstepping/RHO | |
| Praveen et al. | Flow field on helodeck of a frigate: a review |