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This work describes the implementation of optimization techniques based on control theory for complex aircraft configurations. Here control theory is employed to derive the adjoint differential equati...
In safety of life applications using satellite navigation, the Protection Level (PL) equation translates what is known about the pseudorange errors into a hard bound on the positioning error (the Prot...
A light structure is needed to reduce W0. SFC is the province of the engine manufacturers. The aerodynamic designer should try to maximize VL D . This means the cruising speed V should be increase...
While aircraft environmental performance has been important since the beginnings of commercial aviation, continuously increasing passenger traffic and a rise in public awareness have made aircr...
The focus of the present study is to determine the feasibility of including noise and emissions constraints in the early design of the aircraft and mission. This paper introduces the design tool and...
The practical use of high-fidelity multidisciplinary optimization techniques in low-boom supersonic business-jet designs has been limited because of the high computational cost associated with ...
While ATC was originally developed for object-based decomposition, it is also applicable to multidisciplinary design problems. In this paper, both methods are applied to a set of test cases.
This paper provides an introduction to a new method for distributed optimization based on collaborative optimization, a decomposition-based method for the optimization of complex multidisciplinary de...
The 6th Competition of Trajectory Optimization of China (CTOC) (the former Competition of Deep Space Trajectory Optimization of China) is held by the Chinese= Society of Theoretical and Applied Mechan...
The optimization method of a mathematical model and connected-pipe experimental technique for a test in altitude test facility (ATF) of a liquid fuel ramjet engine was researched.The optimization of t...

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