Mimasu et al., 2015 - Google Patents
Attitude Control of Hayabusa2 by Solar Radiation Pressure in One Wheel Control ModeMimasu et al., 2015
View PDF- Document ID
- 8493454391150671195
- Author
- Mimasu Y
- Ono G
- Akatsuka K
- Terui F
- Ogawa N
- Saiki T
- Tsuda Y
- Publication year
- Publication venue
- 25th International Symposium on Space Flight Dynamics
External Links
Snippet
The asteroid explorer Hayabusa2 was launched by Japan Aerospace Exploration Agency (JAXA) on December 3, 2014. During the cruise phase, Hayabusa2 controls its attitude by only one reaction wheel to bias the momentum around Z-axis of the body in order to save …
- 238000006243 chemical reaction 0 abstract description 15
Classifications
-
- 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
- B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun 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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/281—Spin-stabilised spacecraft
-
- 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
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
-
- 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
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
-
- 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
- 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
- B64G2001/245—Spacecraft attitude control, e.g. attitude control algorithms
-
- 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
- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
-
- 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
- B64G1/222—Appendage deployment mechanisms
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/646—Docking or rendez-vous systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
- B64G1/1014—Navigation satellites
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Tsuda et al. | Generalized attitude model for spinning solar sail spacecraft | |
Macdonald et al. | Solar polar orbiter: a solar sail technology reference study | |
JP2010105659A (en) | Method and system for unloading inertia wheel in spacecraft | |
Ran et al. | Attitude control system design and on-orbit performance analysis of nano-satellite—“Tian Tuo 1” | |
Ono et al. | Generalized attitude model for momentum-biased solar sail spacecraft | |
EP0934196A4 (en) | REORIENTATION OF A SPACE ENGINE FROM ITS INITIAL MONOAXIAL ORIENTATION | |
CN105511493A (en) | Low-orbit constellation disposition method based on assistance of martian atmosphere | |
Macdonald et al. | Technology requirements of exploration beyond Neptune by solar sail propulsion | |
Cai et al. | Solar sailing trajectory optimization with planetary gravity assist | |
Lafleur et al. | Low-earth-orbit constellation phasing using miniaturized low-thrust propulsion systems | |
Mimasu et al. | Attitude Control of Hayabusa2 by Solar Radiation Pressure in One Wheel Control Mode | |
Kominato et al. | Optical hybrid navigation and station keeping around Itokawa | |
Caillibot et al. | Formation flying demonstration missions enabled by CanX nanosatellite technology | |
Saiki et al. | Attitude operation results of solar sail demonstrator IKAROS | |
He et al. | Time-optimal rendezvous transfer trajectory for restricted cone-angle range solar sails | |
Wie et al. | Attitude and orbit control systems | |
Brown | A GNC Perspective of the Launch and Commissioning of NASA’s New SMAP (Soil Moisture Active Passive) Spacecraft | |
Hadaegh et al. | Initialization of distributed spacecraft for precision formation flying | |
van der Ha et al. | CONTOUR phasing orbits: attitude determination & control concepts and flight results. | |
Mandy et al. | Implementation of satellite formation flight algorithms using SPHERES aboard the international space station | |
Shoer et al. | Conical scanning approach for sun pointing on the cygnss microsatellite | |
Tsuda et al. | SRP-Assisted Fuel-Free Sun Tracking and Its Application to Hayabusa2 | |
Tsuda et al. | Modeling of solar radiation pressure effect for trajectory guidance of spinner solar sailer IKAROS | |
Nieto et al. | The Pioneer anomaly: The data, its meaning, and a future test | |
Yamaguchi et al. | Solar sail force modeling for spinning solar sail using the radiometric tracking data |