Spivey et al., 2018 - Google Patents
Spanwise adaptive wingSpivey et al., 2018
View PDF- Document ID
- 6425192397102519283
- Author
- Spivey D
- Suh P
- Publication year
- Publication venue
- AIAA Aviation 2018
External Links
Snippet
This presentation discusses the NASA Armstrong PTERA-SAW flight simulation. The uses of this simulation are to study the aerodynamic effects of moving outer wing panels in flight, develop a flight control system, flight safety analysis, mission planning, flight envelope …
- 230000003044 adaptive 0 title description 16
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/40—Transmitting means with power amplification using fluid pressure
- B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- 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
- G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
- B64C9/36—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Livne | Aircraft active flutter suppression: State of the art and technology maturation needs | |
Vepa | Flight dynamics, simulation, and control: for rigid and flexible aircraft | |
Heidlauf et al. | Verification Challenges in F-16 Ground Collision Avoidance and Other Automated Maneuvers. | |
Lee et al. | Simulation of helicopter shipboard launch and recovery with time-accurate airwakes | |
Meyer et al. | A formal structure for advanced automatic flight-control systems | |
de Castro | Flying and handling qualities of a fly-by-wire blended-wing-body civil transport aircraft | |
Angelov | Model-based systems engineering of flight control for vtol transition aircraft | |
Cunningham et al. | A generic t-tail transport airplane simulation for high-angle-of-attack dynamics modeling investigations | |
Kim et al. | Review on flight control law technologies of fighter jets for flying qualities | |
Vayalali et al. | Horizontal stabilator utilization for post swashplate failure operation on a UH-60 black hawk helicopter | |
Surmann et al. | Integrated Flight Control System Architecture and Robustness Analysis for a Lift-to-Cruise Aircraft with Incremental Nonlinear Dynamic Inversion | |
Rice et al. | Control performance analysis for autonomous close formation flight experiments | |
Hamissi et al. | A new nonlinear control design strategy for fixed wing aircrafts piloting | |
Spivey et al. | Spanwise adaptive wing | |
Gu et al. | Autonomous formation flight–design and experiments | |
Berg et al. | Destabilize/Stabilize Approach to Experimental Active Flutter Suppression Technology Development | |
Rachman et al. | Non-linear simulation of controller for longitudinal control augmentation system of F-16 using numerical approach | |
Rachman et al. | A mathematical modeling for design and development of control laws for unmanned aerial vehicle (UAV) | |
Lee | Simulation and control of a helicopter operating in a ship airwake | |
Atesoglu et al. | High-alpha flight maneuverability enhancement of a fighter aircraft using thrust-vectoring control | |
Zafirov et al. | Joined-wing test bed UAV | |
Bhardwaj et al. | Design Reference Model Based Maneuverability Phase Planes of Vertical Take-Off and Landing Aircraft | |
Chudoba et al. | Trim Equations of Motion for Aircraft Design: Steady State Straight Line Flight | |
Urnes et al. | Use of propulsion commands to control directional stability of a damaged transport aircraft | |
Baldelli et al. | Unified rational function approximation formulation for aeroelastic and flight dynamics analyses |