@article{oai:jaxa.repo.nii.ac.jp:00031663,
 author = {本間, 正修 and 渡辺, 篤太郎 and 松尾, 弘毅 and HONMA, Masanori and WATANABE, Atsutarou and MATSUO, Hiroki},
 issue = {1_A},
 journal = {東京大学宇宙航空研究所報告},
 month = {Feb},
 note = {観測ロケットのピッチ=ロール・レゾナンスの問題に関連して,若干の仮定の下に共振点付近での機体の運動の解析を行った. また共振状態が持続するロール・ロック=イン現象について,それが起こらないための条件を求め,シミュレーション結果との比較を行った., To guarantee the stable flight of fin-stabilized sounding rockets, care must be taken against the pitch-roll resonance phenomena which may cause, due to the induced large angle of attack, undesirable attitude disturbance or even vehicle destruction. In this paper, behavior of the angle of attack at near resonance region is analyzed under the assumptions that 1. constant acceleration and constant air density, 2. constant velocity and variable air density. As the conditions necessary to avoid the roll lock-in (continuation of resonance) is sought, with simulated results., 資料番号: SA0124657000},
 pages = {167--190},
 title = {小型ロケットのピッチ=ロール レゾナンス},
 volume = {12},
 year = {1976}
}