Mathavaraj et al., 2021 - Google Patents
Satellite formation flying: high precision guidance using optimal and adaptive control techniquesMathavaraj et al., 2021
- Document ID
- 4926996677578979742
- Author
- Mathavaraj S
- Padhi R
- Publication year
External Links
Snippet
Small satellite technology is opening up a new era in space exploration offering reduced cost of launch and maintenance, operational flexibility with on-orbit reconfiguration, redundancy etc. The true power of such missions can be harnessed only from close and …
- 230000015572 biosynthetic process 0 title abstract description 153
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
- B64G1/28—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
-
- 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
- B64G1/42—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
- B64G1/28—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
- B64G1/24—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
- B64G1/40—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
- B64G2001/245—Spacecraft attitude control, e.g. attitude control algorithms
-
- 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
- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Mathavaraj et al. | Satellite formation flying: high precision guidance using optimal and adaptive control techniques | |
| EP3665085B1 (en) | Spacecraft, and control system and method for controlling operation of spacecraft | |
| Schaub et al. | Impulsive feedback control to establish specific mean orbit elements of spacecraft formations | |
| US10967991B2 (en) | Model predictive control of spacecraft | |
| Heiligers et al. | Novel solar-sail mission concepts for high-latitude Earth and lunar observation | |
| Pirat et al. | Toward the autonomous assembly of large telescopes using cubesat rendezvous and docking | |
| Ceriotti et al. | Hybrid solar sail and solar electric propulsion for novel Earth observation missions | |
| Song et al. | Spacecraft formation flying system design and controls for four nanosats mission | |
| Blandino et al. | Feasibility for orbital life extension of a CubeSat in the lower thermosphere | |
| Baig et al. | Light-levitated geostationary cylindrical orbits are feasible | |
| Edlerman et al. | Cluster-keeping algorithms for the satellite swarm sensor network project | |
| Elliott et al. | Impulsive control of formations near invariant tori via local toroidal coordinates | |
| Scharf et al. | Flight-like ground demonstrations of precision maneuvers for spacecraft formations—Part I | |
| Zhao et al. | Multiple spacecraft formation flying control around artificial equilibrium point using propellantless approach | |
| Edlerman et al. | Analysis of nanosatellite formation establishment and maintenance using electric propulsion | |
| Hassani et al. | H∞ and μ synthesis control of virtual structure satellites formation flying | |
| Campbell et al. | Formation flying mission for the UW Dawgstar satellite | |
| Mathavaraj et al. | Satellite Orbital Dynamics | |
| De Florio et al. | Precise autonomous orbit control in low earth orbit | |
| Jeon et al. | Adaptive Smooth Control via Nonsingular Fast Terminal Sliding Modes for Distributed Space Telescope Demonstration Mission by CubeSat Formation Flying | |
| Kumar et al. | Quaternion Based Optimal Controller for Momentum Biased Nadir Pointing Satellite | |
| Shirazi et al. | Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission | |
| Lippe | Optimal Guidance and Control of Spacecraft Swarms in Planetary and Asteroid Orbits | |
| Luo et al. | Heliotropic frozen orbits design for high area-to-mass ratio spacecraft | |
| Mathavaraj et al. | Introduction and Motivation |