ISBN-13: 9783659307782 / Rosyjski / Miękka / 2012 / 232 str.
Kosmicheskaya trosovaya sistema (KTS)- eto sovokupnost' dvukh i bolee KA, soedinennykh dlinnymi nityami-trosami. Natyazheniem trosa mozhno pereraspredelyat' mezhdu kontsevymi telami KTS zapasennuyu mekhanicheskuyu energiyu vsey sistemy, tem samym sushchestvenno izmenyat' orbity KA.Etim manevram predshestvuet nachal'nyy etap razvertyvaniya sistemy iz monolitnogo sostoyaniya putem impul'snogo rastalkivaniya i posleduyushchego razvertyvaniya KTS. Problema zaklyuchaetsya v tom, chto uroven' upravlyayushchikh vozdeystviy na nachal'nom uchastke razvertyvaniya imeet poryadok model'nykh i instrumental'nykh pogreshnostey.Naibolee kritichno eto proyavlyaetsya dlya malykh KA. Dlya resheniya etoy problemy matematicheski obosnovana i na primere zadachi spuska s orbity malogo KA issledovana skhema neupravlyaemogo razvertyvaniya KTS, obespechivayushchaya maksimal'noe izmenenie mekhanicheskoy energii malogo KA. Predstavlena analiticheskaya model' manevrov malogo KA, pozvolyayushchaya reshat' zadachi ballisticheskogo proektirovaniya oblika sistemy spuska. Privedena sistema pokazateley kachestva manevra malogo KA. Kniga adresovana studentam, aspirantam, nauchnym rabotnikam i spetsialistam v oblasti teorii poleta KA i ballisticheskogo proektirovaniya kosmicheskikh sistem.
Kosmicheskaya trosovaya sistema (KTS)- eto sovokupnost dvukh i bolee KA,soedinennykh dlinnymi nityami-trosami. Natyazheniem trosa mozhno pereraspredelyat mezhdu kontsevymi telami KTS zapasennuyu mekhanicheskuyu energiyu vsey sistemy, tem samym sushchestvenno izmenyat orbity KA.Etim manevram predshestvuet nachalnyy etap razvertyvaniya sistemy iz monolitnogo sostoyaniya putem impulsnogo rastalkivaniya i posleduyushchego razvertyvaniya KTS. Problema zaklyuchaetsya v tom, chto uroven upravlyayushchikh vozdeystviy na nachalnom uchastke razvertyvaniya imeet poryadok modelnykh i instrumentalnykh pogreshnostey.Naibolee kritichno eto proyavlyaetsya dlya malykh KA. Dlya resheniya etoy problemy matematicheski obosnovana i na primere zadachi spuska s orbity malogo KA issledovana skhema neupravlyaemogo razvertyvaniya KTS, obespechivayushchaya maksimalnoe izmenenie mekhanicheskoy energii malogo KA. Predstavlena analiticheskaya model manevrov malogo KA, pozvolyayushchaya reshat zadachi ballisticheskogo proektirovaniya oblika sistemy spuska. Privedena sistema pokazateley kachestva manevra malogo KA. Kniga adresovana studentam, aspirantam, nauchnym rabotnikam i spetsialistam v oblasti teorii poleta KA i ballisticheskogo proektirovaniya kosmicheskikh sistem.