Radio Guidance Command Design for Target Angle Correction of Sounding Rocket S-520-RD1
Author:
Affiliation:
1. Japan Aerospace Exploration Agency,Sagamihara,Japan
2. NEC Aerospace Systems, Ltd.,Fuchu,Japan
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10353928/10354079/10354107.pdf?arnumber=10354107
Reference7 articles.
1. Development of a Small-spin-axis Controller and Its Application to a Solar Sail Subpayload Satellite
2. On the recursive formula of rhumb line maneuvers with its applications
3. SS-520 Nano satellite launcher and its flight result;Inatani
4. Sounding rocket SS-520 as a CubeSat launch vehicle
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