[go: up one dir, main page]

Evdokimov et al., 2014 - Google Patents

Landing a descent module on the Vostochnyi launch site after returning from the Moon

Evdokimov et al., 2014

Document ID
3685251208959511054
Author
Evdokimov S
Klimanov S
Korchagin A
Mikrin E
Sikharulidze Y
Tuchin A
Tuchin D
Publication year
Publication venue
Journal of Computer and Systems Sciences International

External Links

Snippet

Results of the boundary value problem solution for determining the trajectory of returning from the lunar orbit and landing on the Vostochnyi launch site are presented. The solution includes the calculation of the required expenditure of the characteristic velocity for forming …
Continue reading at link.springer.com (other versions)

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
    • G05D1/0883—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for space vehicles
    • 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
    • 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
    • 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
    • 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
    • G05D1/12—Target-seeking control
    • 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
    • B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
    • 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

Similar Documents

Publication Publication Date Title
US9874879B2 (en) Model Predictive control of spacecraft
Dukeman Atmospheric ascent guidance for rocket-powered launch vehicles
Deshmukh et al. Investigation of direct force control for aerocapture at Neptune
Noton Spacecraft navigation and guidance
US10934025B2 (en) Model predictive control of spacecraft
Zhang et al. Autonomous guidance for rendezvous phasing based on special-point-based maneuvers
Putnam et al. PredGuid entry guidance for Orion return from low Earth orbit
Evdokimov et al. Landing a descent module on the Vostochnyi launch site after returning from the Moon
Qiu et al. Deep space exploration orbit design departing from circumlunar orbit of lunar base
Petukhov Quasioptimal control with feedback for multiorbit low-thrust transfer between noncoplanar elliptic and circular orbits
Lee et al. Integrated system for autonomous proximity operations and docking
Kos et al. Altair descent and ascent reference trajectory design and initial dispersion analyses
Evdokimov et al. Terminal control algorithm for the downrange motion of a descent module with load factor constraints
Machuca et al. Autonomous navigation and guidance for CubeSats to flyby near-Earth asteroids
Fill et al. Orion's Powered Flight Guidance Burn Options for Near Term Exploration Missions
Xie et al. Autonomous guidance, navigation, and control of spacecraft
Gordienko et al. The use of three-impulse transfer to insert the spacecraft into the high Moon Artificial Satellite orbits
Matsumoto et al. Accurate Real-Time Prediction Guidance Using Numerical Integration for Reentry Spacecraft
Evdokimov et al. Modification of the Terminal Control Algorithm for Descent under “Magnified” Disturbances after Returning from the Moon
Manohar et al. Trajectory reconstruction during thrusting phase of rockets using differential corrections
Samotokhin et al. Analysis of return trajectories from the Moon
Kinstle Orbital Mechanics of John Glenn’s Mercury Atlas (MA-6): Reconstruction through a STEM Project
Abilleira 2011 Mars Science Laboratory Mission Design Overview
Evdokimov et al. Construction of the initial deorbit region for landing at the given place
Li et al. Lunar orbit insertion targeting from the two-segment lunar free-return trajectories