UN Security Council
2002

and integrated circuits for information security, as follows, and other specially designed computer components therefor: 5.A.2.a.9: Designed or modified to use cryptographic techniques to generate channelizing or scrambling codes for "time modulated ultra-wideband" systems. (4) 7.A.3: Inertial Navigation Systems and inertial equipment and components designed therefor: a. Inertial navigation systems (gimballed or strapdown) and in inertial equipment designed for "aircraft", land vehicle or "spacecraft" for attitude, guidance or control, having any of the following characteristics, and components designed therefor: a.1. (Renumbering of current GRL entry 7.A.3.a.) a.2. (Renumbering of current GRL entry 7.A.3.b.) S/RES/1454 (2002) b. Hybrid Inertial Navigation Systems embedded with Global Navigation Satellite System(s) (GNSS) or with "Data-based referenced Navigation" ("DBRN") System(s) for attitude, guidance or control, subsequent to normal alignment, having an INS navigation position accuracy, after loss of GNSS or "DBRN" for a period of up to 4 minutes, of less (better) than 10 metres Circular Error Probable (CEP). (5) 5.A.1.b.8: Radio Intercept/Direction Finding (DF) Equipment/Systems. (6) 5.A.1.b.7: Being broadcast transmitter (e.g. for radio or television) equipment