Kafer, 1982 - Google Patents
Space Shuttle Entry/Landing flight control design descriptionKafer, 1982
- Document ID
- 6605252449132741502
- Author
- Kafer G
- Publication year
- Publication venue
- Guidance and Control Conference
External Links
Snippet
ABSTRACT The Space Shuttle Entry/Landing flight control design is described. The control system is completely digital and utilizes a" fly-by-wire" implementation. The paper presents a summary description of the vehicle, mission, guidance and navigation interface, sensors …
- 230000010006 flight 0 title abstract description 39
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
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- 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
- G05D1/0077—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements using redundant signals or controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
-
- 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
-
- 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
-
- 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
- B64C29/00—Aircraft capable of landing or taking-off vertically
- B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
Similar Documents
Publication | Publication Date | Title |
---|---|---|
LaCr | Application of nonlinear systems inverses to automatic flight control design-System concepts and flight evaluations | |
US8185255B2 (en) | Robust control effector allocation | |
Napolitano et al. | New technique for aircraft flight control reconfiguration | |
Collinson | Fly-by-wire flight control | |
Stougie et al. | Incremental nonlinear dynamic inversion control with flight envelope protection for the flying-V | |
Canin | F-35 high angle of attack flight control development and flight test results | |
Kafer | Space Shuttle Entry/Landing flight control design description | |
Surmann et al. | Integrated Flight Control System Architecture and Robustness Analysis for a Lift-to-Cruise Aircraft with Incremental Nonlinear Dynamic Inversion | |
Zimpfer et al. | Space shuttle GN&C development history and evolution | |
Davidson | Flight control design and test of the joint unmanned combat air system (J-UCAS) X-45A | |
Wise | Applied controls research topics in the aerospace industry | |
Colgren et al. | Effective design of highly maneuverable tailless aircraft | |
Miyazawa et al. | Flight control system for the automatic landing flight experiment | |
Ward et al. | System identification for retrofit reconfigurable control of an F/A-18 aircraft | |
Chetty et al. | Design, development and flight testing of control laws for the Indian Light Combat Aircraft | |
Edinger | The space shuttle ascent flight control system | |
Colgren et al. | To tail or two tails?-The effective design and modeling of yaw control devices | |
Beh et al. | Control law design and flight test results of the experimental aircraft X-31A | |
Cooke | Space Shuttle stability and control test plan | |
Rohlf et al. | X-31 vector system identification-approach and results | |
Clark et al. | High angle-of-attack flight characteristics of the VF-22 | |
Alwi et al. | Piloted sliding mode FTC simulator evaluation for the ELAL Flight 1862 incident | |
Kasnakoglu et al. | Automatic recovery and autonomous navigation of disabled aircraft after control surface actuator jam | |
Minott et al. | Space Shuttle digital flight control system | |
Proctor | Model Predictive Control Synthesis for the Innovative Control Effector Tailless Fighter Aircraft |