Srivastava et al., 2022 - Google Patents
Attitude determination and control system for a leo debris chaser small satelliteSrivastava et al., 2022
- Document ID
- 5397855332612267395
- Author
- Srivastava R
- Sah R
- Das K
- Publication year
- Publication venue
- AIAA SCITECH 2022 Forum
External Links
Snippet
View Video Presentation: https://doi. org/10.2514/6.2022-0519. vid Attitude Determination and Control System (ADCS) is an important subsystem responsible for measuring and controlling the orientation of a satellite. With respect to active debris removal from LEO using …
- 241000282322 Panthera 0 title 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/10—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in preceding groups by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
-
- 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
- G05D1/0883—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for space vehicles
-
- 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
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in preceding groups
- G01C21/24—Navigation; Navigational instruments not provided for in preceding groups specially adapted for cosmonautical navigation
-
- 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
- B64G1/32—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
- B64G1/24—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
- B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
-
- 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
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Searcy et al. | Magnetometer-only attitude determination using novel two-step Kalman filter approach | |
CN104570742B (en) | Feedforward PID (proportion, integration and differentiation) control based rapid high-precision relative pointing control method of noncoplanar rendezvous orbit | |
Srivastava et al. | Attitude determination and control system for a leo debris chaser small satellite | |
Abdelrahman et al. | Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements | |
Srivastava et al. | Attitude and in-orbit residual magnetic moment estimation of small satellites using only magnetometer | |
Abdelrahman et al. | Sigma-point Kalman filtering for spacecraft attitude and rate estimation using magnetometer measurements | |
Auret | Design of an aerodynamic attitude control system for a CubeSat | |
Mashtakov et al. | Attitude determination & control system design for gravity recovery missions like GRACE | |
Cortiella et al. | 3CAT-2: Attitude determination and control system for a GNSS-R earth observation 6U cubesat mission | |
Somov et al. | Health checking autonomous attitude control system of Earth-observing miniature satellite in initial orientation modes | |
Lightsey et al. | Flight results of GPS based attitude control on the REX II spacecraft | |
Lee et al. | Composite adaptive attitude control of asteroid-orbiting spacecraft with regressor integral excitation | |
Ticona et al. | Attitude determination and control system for nadir pointing and detumbling using magnetorquer for 1u bolivian cubesat | |
Hajiyev et al. | Gyroless attitude and rate estimation of small satellites using singular value decomposition and extended Kalman filter | |
Desouky et al. | Improved magnetic attitude control | |
Dang et al. | Rotational and translational integrated control for inner-formation gravity measurement satellite system | |
Gaber et al. | Real-time implementation of a robust simplified intelligent proportional–integral control for CubeSat attitude determination system | |
Chaves-Jiménez et al. | Impact of dynamic coupling between relative orbit and attitude on the estimation of relative dynamics of spacecraft | |
Babcock | CubeSat attitude determination via Kalman filtering of magnetometer and solar cell data | |
Walker et al. | CubeSat attitude determination using low-cost sensors and magnetic field time derivative | |
Mahdi et al. | Attitude determination and control system design of KufaSat | |
Weiss et al. | Inertia-free spacecraft attitude control with reaction-wheel actuation | |
Mulay et al. | Attitude determination and control of Pratham, Indian Institute of Technology Bombay's first student satellite | |
Tassano et al. | An inexpensive attitude determination system for the uruguayan Cubesat, AntelSat | |
You et al. | A Real-Time Simulator for Processor-In-the-Loop Simulation of Small Satellites |