UA96670C2 - Method of forming logic of placing group of spacecraft s into required orbits - Google Patents

Method of forming logic of placing group of spacecraft s into required orbits

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Publication number
UA96670C2
UA96670C2 UAA201005337A UAA201005337A UA96670C2 UA 96670 C2 UA96670 C2 UA 96670C2 UA A201005337 A UAA201005337 A UA A201005337A UA A201005337 A UAA201005337 A UA A201005337A UA 96670 C2 UA96670 C2 UA 96670C2
Authority
UA
Ukraine
Prior art keywords
spacecraft
spacecrafts
mission profile
separation
parking
Prior art date
Application number
UAA201005337A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Александр Евгеньевич Лукьянович
Александр Федорович Кириченко
Геннадий Иванович Бекшаев
Татьяна Александровна Быкова
Original Assignee
Александр Евгеньевич Лукьянович
Александр Федорович Кириченко
Геннадий Иванович Бекшаев
Татьяна Александровна Быкова
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Александр Евгеньевич Лукьянович, Александр Федорович Кириченко, Геннадий Иванович Бекшаев, Татьяна Александровна Быкова filed Critical Александр Евгеньевич Лукьянович
Priority to UAA201005337A priority Critical patent/UA96670C2/en
Publication of UA96670C2 publication Critical patent/UA96670C2/en

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Abstract

The present invention relates to space engineering, design of control systems of carrier rockets. A method of forming a logic of parking spacecrafts into the required orbits consists in use of a main mission profile of spacecraft parking and an additional mission profile for separation of all groups of spacecrafts that is saturated with the most complete set of basic operations for each spacecraft. The basic operations mean the orientation maneuvers of the longitudinal axis of the parking stage, twist, withdrawal of the parking stage from the spacecraft etc. The passage from the main mission profile to the additional mission profile is carried out under conditions of achievement of a functional for separation of one or the first of each group of spacecrafts. Return to the main mission profile is carried out after the separation of the last spacecraft of the group and implementation of all basic operations planned for it, after which the flight continues according to the standard scheme. The numbering spacecrafts is determined by required sequence of their separation. The invention increases efficiency of the entire rocket-space complex in general, and significantly reduces the cost of adapting it to a specific launching.
UAA201005337A 2010-04-30 2010-04-30 Method of forming logic of placing group of spacecraft s into required orbits UA96670C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAA201005337A UA96670C2 (en) 2010-04-30 2010-04-30 Method of forming logic of placing group of spacecraft s into required orbits

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAA201005337A UA96670C2 (en) 2010-04-30 2010-04-30 Method of forming logic of placing group of spacecraft s into required orbits

Publications (1)

Publication Number Publication Date
UA96670C2 true UA96670C2 (en) 2011-11-25

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ID=50839619

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA201005337A UA96670C2 (en) 2010-04-30 2010-04-30 Method of forming logic of placing group of spacecraft s into required orbits

Country Status (1)

Country Link
UA (1) UA96670C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112241177A (en) * 2020-11-06 2021-01-19 北京理工大学 A heuristic spacecraft mission planning method based on timeline state landmarks

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112241177A (en) * 2020-11-06 2021-01-19 北京理工大学 A heuristic spacecraft mission planning method based on timeline state landmarks

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