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Data · dataset · 2025

Data of Gravity Tractor's Simulation

Listed in ScienceDB

This database calculated the close approach deflection diatance of Apophis* for Gravity Tractor under different warning times (2030~2049). 2 scenarios: static hovering GT and diaplaced orbit GT for S and C type's virtual impactor Apophis* was considered, and recorded results in close apporach deflection disdance.xlsx.

Description

We wrote programs by MATLAB, using high precision ephemeris orbit dynamical model and GA+SQP algorithm, researched the full mission process from “Launch–Transfer–Rendezvous–Deflec­tion–Evaluation” con­strained by launch capacity and warn­ing times.

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Where it is published

Catalogue records · 1

Topics

Inferred from text
Simulation 75%
Provenance · 1 source records, 11 field assertions
SourceKeyLast seenRaw
ScienceDB10.57760/sciencedb.space.023889 d agoJSON v1
FieldAssertionExtractorEvidence
access_levelsource · scidb cnconnector:scidb_cn@1.0.0
concepts[field].local:field:earth-environmentalmapping · scidb cnconnector:scidb_cn@1.0.0
concepts[field].local:field:engineeringmapping · scidb cnconnector:scidb_cn@1.0.0
concepts[field].local:field:humanitiesmapping · scidb cnconnector:scidb_cn@1.0.0
concepts[field].local:field:life-sciencesmapping · scidb cnconnector:scidb_cn@1.0.0
concepts[field].local:field:social-sciencemapping · scidb cnconnector:scidb_cn@1.0.0
concepts[method].local:method:simulationenrichment · scidb cnkeyword-concept-rules@1.0.0title+description (75%)
descriptionsource · scidb cnconnector:scidb_cn@1.0.0/metadata/dc/description
license_textsource · scidb cnconnector:scidb_cn@1.0.0
publication_datesource · scidb cnconnector:scidb_cn@1.0.0
titlesource · scidb cnconnector:scidb_cn@1.0.0/metadata/dc/title