Aircraft Engineering and Aerospace Technology: Volume 78 Issue 5
Strapline:
An International JournalTable of contents
Researches on optimization of micro‐core attitude parameters
Sun Jie, Zhao Yang, Sun Zhaowei, An NanTo provide a new method to determine parameters of the attitude determination system facing micro‐core.
Spacecraft vibration reduction using pulse modulated command input and smart materials
Qinglei HuTo provide an approach to active vibration reduction of flexible spacecraft actuated by on‐off thrusters during attitude control for spacecraft designers, which can help them…
Gas flow simulation in a micro nozzle
Zhao Yang, Yang Hai WeiTo study the flow character in a micro nozzle.
A study on the efficiency of pulsed plasma thruster (PPT)
Hou Dali, Zhao Wansheng, Kang XiaomingThe pulsed plasma thruster (PPT) is one sort of promising electric thrusters, but the low efficiency is always a big problem for PPT. Many researches have been working on solving…
Design of a supervisory controller for CLOS guidance with lead angle
Hadi Nobahari, Aria Alasty, Seid H. PourtakdoustThe purpose of this paper is to propose a supervisory command‐to‐line‐of‐sight guidance law with lead angle which keeps the missile flight within the tracking beam.
Simple autopilot design procedure based on a factorization approach
Amir Nassirharand, Mohammad Hosain AlizadehThe purpose of this paper is to apply a factorization‐based control system design procedure to design of auto‐pilot systems.
Iterative solution to differential geometric guidance problem
Chaoyong Li, Wuxing Jing, Hui Wang, Zhiguo QiTo study the application of three‐dimensional differential geometric (DG) guidance commands to a realistic missile defense engagement, and the application of the Newton's…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb